P. de Vos
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53 records found
1
Exhaust aftertreatment for diesel-methanol dual-fuel marine engines
Kinetic model based verification of a diesel oxidation catalyst for methanol and formaldehyde abatement
The model is a 1D, isothermal, steady-state single-channel plug-flow reactor implemented in Cantera [3] as a chain of 200 Continuous-Stirred Tank Reactors (CSTRs) in series. Internal washcoat diffusion is treated explicitly via the Knudsen-regime effective diffusivity and flat-slab Thiele modulus, resulting in a per-slice, per-species effectiveness-factor multiplier. Axial dispersion, external mass transfer and thermal effects are excluded; external mass transfer is instead absorbed into a calibrated catalytic area parameter (Acat/L), fitted against the original Koop and Deutschmann profiles. The two lumped pre-exponentials were calibrated against experimental methanol data (Chantaravitoon, Chavadej, and Schwank) and the Torkashvand et al. formaldehyde mechanism.
Applied to a representative DMDF exhaust gas composition from Liu et al., the model shows the dual-fuel case needs roughly 1.3× the reactor length of diesel-only operation to reach full conversion. Crucially, when total hydrocarbon concentrations are matched, the two cases converge: the longer length is driven by the much higher methanol inlet concentration, not by any intrinsic disadvantage of methanol oxidation. A sensitivity study identifies Acat/L and the methanol pre-exponential as the dominant uncertainty sources, with the formaldehyde pre-exponential significant only in the dual-fuel case.
The thesis concludes that the doubled-design catalyst is likely sufficient for reducing methanol and formaldehyde to acceptable levels at the studied operating points, providing the first numerical basis for a previously unverified design. Key limitations include the decoupling of washcoat thickness from catalytic area (so thicker washcoat unphysically slows conversion), the isothermal assumption, the lumped rather than elementary treatment of methanol/formaldehyde, and the lack of experimental validation, which was identified as the most critical next step, alongside non-isothermal modelling and explicit external mass transfer. ...
The model is a 1D, isothermal, steady-state single-channel plug-flow reactor implemented in Cantera [3] as a chain of 200 Continuous-Stirred Tank Reactors (CSTRs) in series. Internal washcoat diffusion is treated explicitly via the Knudsen-regime effective diffusivity and flat-slab Thiele modulus, resulting in a per-slice, per-species effectiveness-factor multiplier. Axial dispersion, external mass transfer and thermal effects are excluded; external mass transfer is instead absorbed into a calibrated catalytic area parameter (Acat/L), fitted against the original Koop and Deutschmann profiles. The two lumped pre-exponentials were calibrated against experimental methanol data (Chantaravitoon, Chavadej, and Schwank) and the Torkashvand et al. formaldehyde mechanism.
Applied to a representative DMDF exhaust gas composition from Liu et al., the model shows the dual-fuel case needs roughly 1.3× the reactor length of diesel-only operation to reach full conversion. Crucially, when total hydrocarbon concentrations are matched, the two cases converge: the longer length is driven by the much higher methanol inlet concentration, not by any intrinsic disadvantage of methanol oxidation. A sensitivity study identifies Acat/L and the methanol pre-exponential as the dominant uncertainty sources, with the formaldehyde pre-exponential significant only in the dual-fuel case.
The thesis concludes that the doubled-design catalyst is likely sufficient for reducing methanol and formaldehyde to acceptable levels at the studied operating points, providing the first numerical basis for a previously unverified design. Key limitations include the decoupling of washcoat thickness from catalytic area (so thicker washcoat unphysically slows conversion), the isothermal assumption, the lumped rather than elementary treatment of methanol/formaldehyde, and the lack of experimental validation, which was identified as the most critical next step, alongside non-isothermal modelling and explicit external mass transfer.
AmmoniaDrive ship integration
A case study on the design of an Ammonia SOFC-ICE power generation system in a car carrier
In AmmoniaDrive, ammonia is used in as the primary fuel for the SOFC system to generate electrical power. The remaining hydrogen-rich anode off-gas is subsequently used as a combustion enhancer in the ammonia-fuelled ICE. The electrical power is used for auxiliary loads and supports propulsion through an electrical machine, while the ICE provides the main propulsion power.
A car carrier was selected as the reference ship due to its standard route, predictable operating profile, high-value cargo, and potential ammonia bunkering at fixed ports. The base-case ship has a length of 199.9 m, a beam of 36.5 m, a service speed of 18 kn, and a cargo capacity of approximately 8,000 CEU and AmmoniaDrive was integrated into the base case without changing the main dimensions and while keeping the operating profile the same.
The results show that AmmoniaDrive can be technically integrated into a car carrier, but not just as a direct replacement for a conventional diesel propulsion system. The main design changes are caused by the ammonia storage and the ammonia power plant. To maintain the required round-trip autonomy, including reserve, the volume occupied by the tank quadruples with respect to the base case. Consequently, the available car deck area decreases by 7.40%.
AmmoniaDrive is a technically feasible concept for car carriers, provided that the ship is designed around the ammonia fuel system. Its feasibility is mainly governed by the cargo capacity loss, emission reduction potential, fuel autonomy, and the technology maturity.
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In AmmoniaDrive, ammonia is used in as the primary fuel for the SOFC system to generate electrical power. The remaining hydrogen-rich anode off-gas is subsequently used as a combustion enhancer in the ammonia-fuelled ICE. The electrical power is used for auxiliary loads and supports propulsion through an electrical machine, while the ICE provides the main propulsion power.
A car carrier was selected as the reference ship due to its standard route, predictable operating profile, high-value cargo, and potential ammonia bunkering at fixed ports. The base-case ship has a length of 199.9 m, a beam of 36.5 m, a service speed of 18 kn, and a cargo capacity of approximately 8,000 CEU and AmmoniaDrive was integrated into the base case without changing the main dimensions and while keeping the operating profile the same.
The results show that AmmoniaDrive can be technically integrated into a car carrier, but not just as a direct replacement for a conventional diesel propulsion system. The main design changes are caused by the ammonia storage and the ammonia power plant. To maintain the required round-trip autonomy, including reserve, the volume occupied by the tank quadruples with respect to the base case. Consequently, the available car deck area decreases by 7.40%.
AmmoniaDrive is a technically feasible concept for car carriers, provided that the ship is designed around the ammonia fuel system. Its feasibility is mainly governed by the cargo capacity loss, emission reduction potential, fuel autonomy, and the technology maturity.
Part-load operation of an ammonia-fuelled SOFC-ICE combined system
Applied to the operational profile of a large container vessel as a case study
A more novel propulsion concept is the use of Solid Oxide Fuel Cells (SOFCs), which electrochemically oxidize hydrogen to generate electricity with high efficiency and very low emissions. Hydrogen is produced by cracking ammonia at the high operating temperatures of the SOFC. However, SOFCs cannot utilize all supplied fuel without complex recirculation, resulting in an anode-off-gas (AOG) that still contains hydrogen.
Because ICEs provide higher power density, better transient response, and lower investment costs than SOFCs, combining both technologies is an attractive solution. In the AmmoniaDrive concept, ammonia is converted efficiently into electricity by the SOFC, while hydrogen in the SOFC anode-off-gas enhances ammonia combustion in the ICE. This hybrid configuration combines the efficiency of SOFCs with the operational flexibility of ICEs.
This study investigates the application of the AmmoniaDrive concept to a 14,000 TEU container vessel. The propulsion system consists of a low-speed two-stroke main engine directly driving the propeller, combined with an electric machine that enables power take-off (PTO), power take-in (PTI), and SOFC-only operation. The SOFC operates continuously, supplying electrical power during sailing, anchoring, and port stays. The system is evaluated for a voyage from Rotterdam to Shanghai via the Suez Canal, including four days in port or at anchor. Simulations consider high and low electrical power demand and three nominal power splits of 16.3%, 21.4%, and 30.4%.
The operational profile is simulated using a Matlab/Simulink model based on earlier work on the AmmoniaDrive concept. The original full-load model was extensively modified to simulate part-load operation of both the SOFC and the ICE. The SOFC model incorporates NTU-based heat exchangers, load-independent heat losses, a minimum cathode airflow, improved temperature control, and an optimized external ammonia cracking strategy using combustion of part of the anode-off-gas. The ICE model retains the five-point Seiliger cycle while incorporating load- and speed-dependent losses, auxiliary blowers for low-load operation, and electric machine models for hybrid power delivery.
The hybrid propulsion system is compared with a conventional reference system consisting of a main engine and generator sets. Fuel consumption is reduced by approximately 10%, 13%, and 16% for the low, medium, and high nominal power split configurations, respectively. Combined system efficiencies generally range from 55% to 70%, with higher power splits and lower propulsion loads resulting in better performance. System efficiency is primarily influenced by SOFC load, ICE load, operational power split, external cracking ratio, and fuel utilization.
Optimal SOFC load is generally between 85% and 100% at high sailing speeds, while the ICE supplies most transient power demand. At lower sailing speeds, SOFC load decreases only slightly, although electric machine limitations may restrict operation. Estimated NOx emissions decrease by 21–39%, depending mainly on the nominal power split. Although these estimates are based on published engine test-cycle data and do not account for hydrogen-ammonia combustion or part-load effects, a substantial reduction in NOx emissions is expected.
An alternative operating strategy, in which the SOFC continuously operates at full load while the ICE supplies all power variations, increases total fuel consumption by only 0.52% on average and slightly reduces NOx emissions. This strategy may improve load-following capability and reduce SOFC degradation. The study demonstrates that ammonia-fuelled SOFC-ICE hybrid systems can efficiently propel large container vessels under varying operating conditions, achieving fuel savings of 10–16% while providing a promising pathway towards cost-effective, CO₂-free shipping. ...
A more novel propulsion concept is the use of Solid Oxide Fuel Cells (SOFCs), which electrochemically oxidize hydrogen to generate electricity with high efficiency and very low emissions. Hydrogen is produced by cracking ammonia at the high operating temperatures of the SOFC. However, SOFCs cannot utilize all supplied fuel without complex recirculation, resulting in an anode-off-gas (AOG) that still contains hydrogen.
Because ICEs provide higher power density, better transient response, and lower investment costs than SOFCs, combining both technologies is an attractive solution. In the AmmoniaDrive concept, ammonia is converted efficiently into electricity by the SOFC, while hydrogen in the SOFC anode-off-gas enhances ammonia combustion in the ICE. This hybrid configuration combines the efficiency of SOFCs with the operational flexibility of ICEs.
This study investigates the application of the AmmoniaDrive concept to a 14,000 TEU container vessel. The propulsion system consists of a low-speed two-stroke main engine directly driving the propeller, combined with an electric machine that enables power take-off (PTO), power take-in (PTI), and SOFC-only operation. The SOFC operates continuously, supplying electrical power during sailing, anchoring, and port stays. The system is evaluated for a voyage from Rotterdam to Shanghai via the Suez Canal, including four days in port or at anchor. Simulations consider high and low electrical power demand and three nominal power splits of 16.3%, 21.4%, and 30.4%.
The operational profile is simulated using a Matlab/Simulink model based on earlier work on the AmmoniaDrive concept. The original full-load model was extensively modified to simulate part-load operation of both the SOFC and the ICE. The SOFC model incorporates NTU-based heat exchangers, load-independent heat losses, a minimum cathode airflow, improved temperature control, and an optimized external ammonia cracking strategy using combustion of part of the anode-off-gas. The ICE model retains the five-point Seiliger cycle while incorporating load- and speed-dependent losses, auxiliary blowers for low-load operation, and electric machine models for hybrid power delivery.
The hybrid propulsion system is compared with a conventional reference system consisting of a main engine and generator sets. Fuel consumption is reduced by approximately 10%, 13%, and 16% for the low, medium, and high nominal power split configurations, respectively. Combined system efficiencies generally range from 55% to 70%, with higher power splits and lower propulsion loads resulting in better performance. System efficiency is primarily influenced by SOFC load, ICE load, operational power split, external cracking ratio, and fuel utilization.
Optimal SOFC load is generally between 85% and 100% at high sailing speeds, while the ICE supplies most transient power demand. At lower sailing speeds, SOFC load decreases only slightly, although electric machine limitations may restrict operation. Estimated NOx emissions decrease by 21–39%, depending mainly on the nominal power split. Although these estimates are based on published engine test-cycle data and do not account for hydrogen-ammonia combustion or part-load effects, a substantial reduction in NOx emissions is expected.
An alternative operating strategy, in which the SOFC continuously operates at full load while the ICE supplies all power variations, increases total fuel consumption by only 0.52% on average and slightly reduces NOx emissions. This strategy may improve load-following capability and reduce SOFC degradation. The study demonstrates that ammonia-fuelled SOFC-ICE hybrid systems can efficiently propel large container vessels under varying operating conditions, achieving fuel savings of 10–16% while providing a promising pathway towards cost-effective, CO₂-free shipping.
Interpretation of the existing literature mainly results in the usage of a spark-ignited ICE, an external ammonia cracker and a battery as ESS. It also becomes evident that the ICE-SOFC installed power ratio is an important factor, as the SOFC and ICE differ in design and operational characteristics. To obtain further case-specific implications, a time-based simulation approach is adopted. The purpose of the simulation is to investigate the effect of component sizing, to develop an energy management system and to analyse the performance of the system. A thermodynamic analysis of the system and scaling towards the desired operational profile are initially performed. The SOFC is then simulated through a 0D thermodynamic model, and the ICE is modelled too, with the help of a Mean Value Engine Model (MVEM), using a Seiliger cycle. The battery is subsequently simulated with a medium pass filter, concluding with the development of a rule-based energy management strategy. The design-related analysis is based on the following Key Performance Indicators (KPIs): the required energy capacity of the battery and the required onboard space for the drivetrain. While for the operations, the following KPI are assessed: the average system fuel efficiency, the correct balancing of the hydrogen flow, the compliance with the demanded energy during a dredging cycle and the safe operations of the battery.
For the application of the ICE-SOFC system on a TSHD with a capacity of 25.000 m3, it can be concluded that a battery size of 10.0 MWh for the 50-50 ICE-SOFC configuration is required. The required capacity decreases, almost linearly, with increased installed ICE fractions, towards 4.38 MWh in the 80-20 ICE-SOFC configuration. The subsequent volume needed to integrate the ammonia-fuelled drivetrain shows a clear trend; at configuration with the power production ratio of 50-50 ICE-SOFC, the needed space is the largest. When the conclusions with regards to the operations are addressed, it can be stated that the operational profile of the TSHD can be managed by the ammonia-fuelled system. This holds for all the assessed configurations, if the system is controlled by the developed rule-based strategy. While supplying the demanded energy during operations, the integrated ICE-SOFC system shows an average system efficiency ranging from 43.8% towards 45.8%, at varying installed power ratios. When the power production ratio favours the SOFC, the total system efficiency increases. The average supply of hydrogen by the SOFC and average demand of hydrogen by the ICE can be balanced during operations, in each discussed configuration. When the battery performance is assessed, the safety limits of the State of Charge (SoC) and discharge/charge power are never crossed, showing that correct usage for each installed power ratio is possible. All in all, this research contributes towards a better understanding of the application of ammonia as a fuel in TSHDs. Further research is however still required to clarify the exact potential of this technology.
...
Interpretation of the existing literature mainly results in the usage of a spark-ignited ICE, an external ammonia cracker and a battery as ESS. It also becomes evident that the ICE-SOFC installed power ratio is an important factor, as the SOFC and ICE differ in design and operational characteristics. To obtain further case-specific implications, a time-based simulation approach is adopted. The purpose of the simulation is to investigate the effect of component sizing, to develop an energy management system and to analyse the performance of the system. A thermodynamic analysis of the system and scaling towards the desired operational profile are initially performed. The SOFC is then simulated through a 0D thermodynamic model, and the ICE is modelled too, with the help of a Mean Value Engine Model (MVEM), using a Seiliger cycle. The battery is subsequently simulated with a medium pass filter, concluding with the development of a rule-based energy management strategy. The design-related analysis is based on the following Key Performance Indicators (KPIs): the required energy capacity of the battery and the required onboard space for the drivetrain. While for the operations, the following KPI are assessed: the average system fuel efficiency, the correct balancing of the hydrogen flow, the compliance with the demanded energy during a dredging cycle and the safe operations of the battery.
For the application of the ICE-SOFC system on a TSHD with a capacity of 25.000 m3, it can be concluded that a battery size of 10.0 MWh for the 50-50 ICE-SOFC configuration is required. The required capacity decreases, almost linearly, with increased installed ICE fractions, towards 4.38 MWh in the 80-20 ICE-SOFC configuration. The subsequent volume needed to integrate the ammonia-fuelled drivetrain shows a clear trend; at configuration with the power production ratio of 50-50 ICE-SOFC, the needed space is the largest. When the conclusions with regards to the operations are addressed, it can be stated that the operational profile of the TSHD can be managed by the ammonia-fuelled system. This holds for all the assessed configurations, if the system is controlled by the developed rule-based strategy. While supplying the demanded energy during operations, the integrated ICE-SOFC system shows an average system efficiency ranging from 43.8% towards 45.8%, at varying installed power ratios. When the power production ratio favours the SOFC, the total system efficiency increases. The average supply of hydrogen by the SOFC and average demand of hydrogen by the ICE can be balanced during operations, in each discussed configuration. When the battery performance is assessed, the safety limits of the State of Charge (SoC) and discharge/charge power are never crossed, showing that correct usage for each installed power ratio is possible. All in all, this research contributes towards a better understanding of the application of ammonia as a fuel in TSHDs. Further research is however still required to clarify the exact potential of this technology.
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This dissertation addresses the growing need for sustainable marine fuels by exploring premixed combustion strategies to adopt methanol in marine engines. Because low reactivity of methanol limits its suitability for conventional compression ignition (CI) diesel engines, alternative premixed combustion concepts emerge. Lean-burn spark-ignition (LBSI) and premixed dual-fuel (PRDF) strategies share a premixed combustion concept and robust ignition control. In addition to new engine design architectures, the ability to convert existing diesel platforms to premixed methanol combustion with only relatively minor modifications makes these concepts highly attractive. Given the long operational lifespan of marine engines, such retrofit capability can smoothen and accelerate maritime defossilization. To inform the development of retrofit and next-generation methanol marine engines, this research offers an in-depth examination of these engine technologies, elucidating their potential and limitations.
The primary objective of this dissertation is to develop an experimentally based thermodynamic analysis framework for premixed methanol engine technologies, linking in-cylinder pressure-based and combustion-informed heat release analysis with engine performance indicators. This framework is tailored to the two premixed concepts of LBSI and PRDF. Building on these frameworks, the overarching goal of the thesis is to enhance the understanding of the performance of methanol-fueled premixed concepts, including their distinct combustion behavior, stability limits, efficiency, and emission characteristics. To this end, the frameworks are applied to two marine engine testbeds through targeted experimental campaigns: 1) a 34.7 liter multi-cylinder LBSI engine, and 2) a 4.1 liter single-cylinder PRDF engine.
To realize this research goal, this dissertation first reviews the research landscape of methanol engines and establishes the conceptual basis for the subsequent analysis frameworks. Beyond conducting a comprehensive literature review and identifying research gaps in SI and PRDF methanol operation, the review clarifies the inconsistent terminology used for injection, ignition, and combustion strategies for methanol use. To further address this, a unified classification framework is proposed that links injection and ignition strategies to combustion modes.
Building on this foundation, this thesis introduces a combustion chamber geometry-and concept-driven combustion characterization framework for LBSI multi-cylinder engines and applies it in experimental campaigns using natural gas as a fuel, as the LBSI engine cannot yet run on methanol. By resolving the distinct combustion phasing and linking it to engine performance indicators, this research shows that advancing the transition point at which the flame enters the squish region improves combustion stability as well as brake thermal and combustion efficiency, albeit with increased heat losses and NOx formation. The experimental framework integrates a multi-stage Wiebe formulation as an additional quantitative diagnostic tool for characterizing dual-stage combustion behavior. Because the combustion-phasing framework is rooted in the premixed flame-propagation dynamics associated with the chamber geometry, rather than in fuel-specific properties only, its qualitative conclusions are expected to remain valid for methanol LBSI operation. To this end, the diagnostic approach is deemed conceptually suited for direct application in future methanol-LBSI engine experiments.
Subsequently, this dissertation proposes a methodological analysis framework tailored to methanol PRDF operation. This framework enables both qualitative and quantitative analysis of heat release profiles and is applied in an experimental campaign on the single-cylinder test engine operating at high methanol energy fractions (MEFs). The qualitative analysis reveals three distinct combustion modes—characterized by m-, h-, and n-shaped profiles—unique to methanol PRDF operation, and associates them with specific underlying mechanisms. A systematic quantitative method based on two heat release morphology indicators—the Combustion Mechanism Index (CMI) and Phase Magnitude Ratio (PMR)—is proposed to map and classify these combustion modes. Methanol PRDF operation achieves lower NOx emissions than diesel-only (DO) baseline operation, but at the expense of higher NO2/NO ratios and substantial rise in CO and UHC emissions. While transitioning from DO to methanol PRDF offers potential efficiency gains for marine engines, especially under high-load operation, combustion losses remain the primary barrier. Building on the investigation of MEF effects and leveraging the developed framework, this thesis explores certain boundary conditions to assess their potential in mitigating methanol PRDF challenges. The parametric analysis of intake temperature and intake/exhaust pressures highlights the critical role of boundary conditions in enabling high-MEF, high-load PRDF operation, especially for diesel engines with mechanically controlled injection. Increasing intake temperature enhances combustion, allowing MEF to reach 93% without significant penalties in heat losses or NOx emissions. Similarly, reducing intake pressure enriches the mixture and improves combustion efficiency without compromising the high temperature related aspects. The morphological analysis during this reduction reveals a transition from h-shaped to bell-shaped heat release profiles, indicating a shift in the dominant combustion mechanism from flame propagation toward premixed autoignition.
On a final note, this dissertation aims not only to advance understanding of premixed methanol combustion in large-bore engines but also to provide practical diagnostic methodologies that support research and development of marine power systems powered by sustainable fuels. Therefore, the developed frameworks are intended to be refined and expanded to other engines and fuels, and as such this thesis contributes to more sustainable shipping. ...
This dissertation addresses the growing need for sustainable marine fuels by exploring premixed combustion strategies to adopt methanol in marine engines. Because low reactivity of methanol limits its suitability for conventional compression ignition (CI) diesel engines, alternative premixed combustion concepts emerge. Lean-burn spark-ignition (LBSI) and premixed dual-fuel (PRDF) strategies share a premixed combustion concept and robust ignition control. In addition to new engine design architectures, the ability to convert existing diesel platforms to premixed methanol combustion with only relatively minor modifications makes these concepts highly attractive. Given the long operational lifespan of marine engines, such retrofit capability can smoothen and accelerate maritime defossilization. To inform the development of retrofit and next-generation methanol marine engines, this research offers an in-depth examination of these engine technologies, elucidating their potential and limitations.
The primary objective of this dissertation is to develop an experimentally based thermodynamic analysis framework for premixed methanol engine technologies, linking in-cylinder pressure-based and combustion-informed heat release analysis with engine performance indicators. This framework is tailored to the two premixed concepts of LBSI and PRDF. Building on these frameworks, the overarching goal of the thesis is to enhance the understanding of the performance of methanol-fueled premixed concepts, including their distinct combustion behavior, stability limits, efficiency, and emission characteristics. To this end, the frameworks are applied to two marine engine testbeds through targeted experimental campaigns: 1) a 34.7 liter multi-cylinder LBSI engine, and 2) a 4.1 liter single-cylinder PRDF engine.
To realize this research goal, this dissertation first reviews the research landscape of methanol engines and establishes the conceptual basis for the subsequent analysis frameworks. Beyond conducting a comprehensive literature review and identifying research gaps in SI and PRDF methanol operation, the review clarifies the inconsistent terminology used for injection, ignition, and combustion strategies for methanol use. To further address this, a unified classification framework is proposed that links injection and ignition strategies to combustion modes.
Building on this foundation, this thesis introduces a combustion chamber geometry-and concept-driven combustion characterization framework for LBSI multi-cylinder engines and applies it in experimental campaigns using natural gas as a fuel, as the LBSI engine cannot yet run on methanol. By resolving the distinct combustion phasing and linking it to engine performance indicators, this research shows that advancing the transition point at which the flame enters the squish region improves combustion stability as well as brake thermal and combustion efficiency, albeit with increased heat losses and NOx formation. The experimental framework integrates a multi-stage Wiebe formulation as an additional quantitative diagnostic tool for characterizing dual-stage combustion behavior. Because the combustion-phasing framework is rooted in the premixed flame-propagation dynamics associated with the chamber geometry, rather than in fuel-specific properties only, its qualitative conclusions are expected to remain valid for methanol LBSI operation. To this end, the diagnostic approach is deemed conceptually suited for direct application in future methanol-LBSI engine experiments.
Subsequently, this dissertation proposes a methodological analysis framework tailored to methanol PRDF operation. This framework enables both qualitative and quantitative analysis of heat release profiles and is applied in an experimental campaign on the single-cylinder test engine operating at high methanol energy fractions (MEFs). The qualitative analysis reveals three distinct combustion modes—characterized by m-, h-, and n-shaped profiles—unique to methanol PRDF operation, and associates them with specific underlying mechanisms. A systematic quantitative method based on two heat release morphology indicators—the Combustion Mechanism Index (CMI) and Phase Magnitude Ratio (PMR)—is proposed to map and classify these combustion modes. Methanol PRDF operation achieves lower NOx emissions than diesel-only (DO) baseline operation, but at the expense of higher NO2/NO ratios and substantial rise in CO and UHC emissions. While transitioning from DO to methanol PRDF offers potential efficiency gains for marine engines, especially under high-load operation, combustion losses remain the primary barrier. Building on the investigation of MEF effects and leveraging the developed framework, this thesis explores certain boundary conditions to assess their potential in mitigating methanol PRDF challenges. The parametric analysis of intake temperature and intake/exhaust pressures highlights the critical role of boundary conditions in enabling high-MEF, high-load PRDF operation, especially for diesel engines with mechanically controlled injection. Increasing intake temperature enhances combustion, allowing MEF to reach 93% without significant penalties in heat losses or NOx emissions. Similarly, reducing intake pressure enriches the mixture and improves combustion efficiency without compromising the high temperature related aspects. The morphological analysis during this reduction reveals a transition from h-shaped to bell-shaped heat release profiles, indicating a shift in the dominant combustion mechanism from flame propagation toward premixed autoignition.
On a final note, this dissertation aims not only to advance understanding of premixed methanol combustion in large-bore engines but also to provide practical diagnostic methodologies that support research and development of marine power systems powered by sustainable fuels. Therefore, the developed frameworks are intended to be refined and expanded to other engines and fuels, and as such this thesis contributes to more sustainable shipping.
Integrating alternative fuels in a patrol vessel fleet
Adopting alternative climate neutral energy carriers to contribute to an environmentally friendly future
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A comprehensive literature review highlights hydrogen's unique combustion characteristics, such as high flame speeds, low ignition energy, and wide flammability range, along with associated challenges like pre-ignition, knocking, and NOx emissions. Existing combustion strategies and injection technologies, particularly those adapted from natural gas-fueled engines, are evaluated for their applicability to hydrogen combustion.
The developed combustion model integrates a Seiliger cycle representation enhanced by temperature-dependent thermodynamic properties. It systematically assesses the effects of hydrogen combustion on key engine parameters, including pressure rise rate, peak cylinder pressures, and temperatures, under various operational scenarios. The results highlight the importance of combustion phasing and air-excess ratios in managing hydrogen combustion characteristics, indicating that careful optimisation of injection timing and combustion strategy is crucial to ensure safe and efficient engine operation. Although the model reveals risks associated with aggressive combustion scenarios, such as exceeding mechanical design limits due to high peak pressures, it provides a structured framework for identifying realistic operating conditions for hydrogen LPDI combustion.
This research thus offers critical insights into the technical feasibility and practical limitations of hydrogen combustion in large two-stroke marine engines, contributing valuable guidance for future development and experimental validation efforts. ...
A comprehensive literature review highlights hydrogen's unique combustion characteristics, such as high flame speeds, low ignition energy, and wide flammability range, along with associated challenges like pre-ignition, knocking, and NOx emissions. Existing combustion strategies and injection technologies, particularly those adapted from natural gas-fueled engines, are evaluated for their applicability to hydrogen combustion.
The developed combustion model integrates a Seiliger cycle representation enhanced by temperature-dependent thermodynamic properties. It systematically assesses the effects of hydrogen combustion on key engine parameters, including pressure rise rate, peak cylinder pressures, and temperatures, under various operational scenarios. The results highlight the importance of combustion phasing and air-excess ratios in managing hydrogen combustion characteristics, indicating that careful optimisation of injection timing and combustion strategy is crucial to ensure safe and efficient engine operation. Although the model reveals risks associated with aggressive combustion scenarios, such as exceeding mechanical design limits due to high peak pressures, it provides a structured framework for identifying realistic operating conditions for hydrogen LPDI combustion.
This research thus offers critical insights into the technical feasibility and practical limitations of hydrogen combustion in large two-stroke marine engines, contributing valuable guidance for future development and experimental validation efforts.
Dual Fuel combustion of Methanol and PODE in a marine ICE and on-board production of PODE
Modelling of a process plant design and engine system
Ammonia (NH3) has unfavorable properties for combustion, such as a high heat of vaporization, narrow flammability limits, a high flame quenching distance, low flame speed, and most important: a high resistance to autoignition. Those properties have to be overcome and hydrogen (H2) is known to be capable of playing a role. As the properties of hydrogen are extremely high combustion speed, very wide flammability limits and a very short flame quenching distance. Unfortunately, both ammonia and hydrogen have a high resistance to autoignition, while CI engines need a fuel with low resistance to auto-ignition. For this reason, a carbon-based fuel, like DME or HVO, is considered necessary to achieve ignition.
The state-of-the-art experimentally achieved combustion concepts are an homogeneous charge compression ignition (HCCI) combustion concept of Pochet et al. [2020a] and an reactivity controlled compression ignition (RCCI) combustion concept of Chiera et al. [2022]. The HCCI combustion concept is fueled by NH3 and H2, without a carbon-based fuel. However, it requires a compression ratio (CR) of 22, a high intake temperature, and is limited by the maximum pressure rise rate (MPRR). The RCCI combustion concept is fueled by NH3 and diesel. This concept can achieve up to 81%e NH3, but still requires 19%e diesel.
A modeling study is done to investigate how to improve the CI combustion strategies, taking into consideration the context of AmmoniaDrive. The modeling study consists of two closed volume single-zone thermodynamic reactor models: the ignition model and the engine cylinder model. The ignition model is a constant volume model, resembling top dead center (TDC) conditions. The engine cylinder model simulates a closed volume from bottom dead center (BDC) to 90 CAD after TDC and incorporates volume change and the heat loss. Bothmodels make use of the chemical kinetic mechanism of Shrestha et al. [2018] to incorporate the combustion reaction. Due to the limitation imposed by the available species in chemical kinetic mechanisms, the carbon-based fuel in the modeling study is DME. For the future, hydrotreated vegetable oil (HVO) seems a more favorable carbon-based fuel, based on experimental results in a constant volume combustion chamber (CVCC) of Hernandez et al. [2023].
The results of the two models indicate that an HCCI combustion concept of ammonia and hydrogen, without a carbon-based fuel, will not ignite within the engine limits of the AmmoniaDrive test engine. An HCCI combustion concept of ammonia, hydrogen, with DME will ignite, but has a limited power output due to the MPRR. An RCCI combustion concept with stratification of DME throughout the cylinder looks promising based on the engine cylinder model results. Stratifying DME concentration, and with that the fuel reactivity, is likely to reduce the MPRR. This would allow for a higher power output due to the possibility to injectmore fuel energy without exceeding the engine limits.
Combining the literature and modeling results, it is likely that an RCCI combustion concept with ammonia, hydrogen, and HVO will lead to a higher power output and a decreased required amount of carbon-based fuel, whilst staying within engine limits. ...
Ammonia (NH3) has unfavorable properties for combustion, such as a high heat of vaporization, narrow flammability limits, a high flame quenching distance, low flame speed, and most important: a high resistance to autoignition. Those properties have to be overcome and hydrogen (H2) is known to be capable of playing a role. As the properties of hydrogen are extremely high combustion speed, very wide flammability limits and a very short flame quenching distance. Unfortunately, both ammonia and hydrogen have a high resistance to autoignition, while CI engines need a fuel with low resistance to auto-ignition. For this reason, a carbon-based fuel, like DME or HVO, is considered necessary to achieve ignition.
The state-of-the-art experimentally achieved combustion concepts are an homogeneous charge compression ignition (HCCI) combustion concept of Pochet et al. [2020a] and an reactivity controlled compression ignition (RCCI) combustion concept of Chiera et al. [2022]. The HCCI combustion concept is fueled by NH3 and H2, without a carbon-based fuel. However, it requires a compression ratio (CR) of 22, a high intake temperature, and is limited by the maximum pressure rise rate (MPRR). The RCCI combustion concept is fueled by NH3 and diesel. This concept can achieve up to 81%e NH3, but still requires 19%e diesel.
A modeling study is done to investigate how to improve the CI combustion strategies, taking into consideration the context of AmmoniaDrive. The modeling study consists of two closed volume single-zone thermodynamic reactor models: the ignition model and the engine cylinder model. The ignition model is a constant volume model, resembling top dead center (TDC) conditions. The engine cylinder model simulates a closed volume from bottom dead center (BDC) to 90 CAD after TDC and incorporates volume change and the heat loss. Bothmodels make use of the chemical kinetic mechanism of Shrestha et al. [2018] to incorporate the combustion reaction. Due to the limitation imposed by the available species in chemical kinetic mechanisms, the carbon-based fuel in the modeling study is DME. For the future, hydrotreated vegetable oil (HVO) seems a more favorable carbon-based fuel, based on experimental results in a constant volume combustion chamber (CVCC) of Hernandez et al. [2023].
The results of the two models indicate that an HCCI combustion concept of ammonia and hydrogen, without a carbon-based fuel, will not ignite within the engine limits of the AmmoniaDrive test engine. An HCCI combustion concept of ammonia, hydrogen, with DME will ignite, but has a limited power output due to the MPRR. An RCCI combustion concept with stratification of DME throughout the cylinder looks promising based on the engine cylinder model results. Stratifying DME concentration, and with that the fuel reactivity, is likely to reduce the MPRR. This would allow for a higher power output due to the possibility to injectmore fuel energy without exceeding the engine limits.
Combining the literature and modeling results, it is likely that an RCCI combustion concept with ammonia, hydrogen, and HVO will lead to a higher power output and a decreased required amount of carbon-based fuel, whilst staying within engine limits.
Ammonia needs to be handled, stored and consumed taking into account safety precautions to have a safe operable ship. Additionally, ammonia has poor combustion characteristics, and therefore a promoter such as hydrogen (7-11%) or MGO (40-60%) is necessary to initiate the combustion. Additionally, internal combustion engines (ICE) using ammonia as a fuel are expected to have a low transient load capability. Therefore, if there is no MGO present, the dynamic loading capability of the ICE with the load variation of the dredging process is a challenge. The same challenge applies for a Solid oxide fuel cell (SOFC), where the SOFC does hardly have transient load capabilities.
A TSHD currently has an ICE capable of dynamic loading, and the main reasons for this transient load is the change in propulsion power, which is dependent on the friction of the draghead and the sailing speed of the vessel. Furthermore, a sudden change in mixture density in the dredging tube during dredging will result in a sudden transient load. To cope with these transient loads, the energy supply on board of a TSHD must have transient load capabilities.
A fuel consumption model has been developed to compare five drive train configurations for the dredging project Kustlijnzorg with an operational profile of 30 days with respect to the original drivetrain. The total power demand [kW] and the transient load [kW/s] was included on a boolean way in this model. When the power demand or the transient load was too high then the model would stop. By means of this model, the main particulars of the engines, fuel cells and batteries regarding power and energy were determined. The output of this model was the amount of fuel consumed during 30 days. This fuel consumption model was validated with another project.
The Construction Industry Research and Information Association (CIRIA) has developed a method to valuate a TSHD. With this CIRIA methods, the value of a conventional TSHD is determined and compared with the value of the ammonia driven configurations. The value of a new vessel that operates on ammonia can be estimated with the help of a sustainability factor. It is found that the weekly cost of the vessel is mainly dependent on; the value of the vessel, which is dependent on the installed power and cost of technology, the fuel consumption, the cost of fuel and the carbon tax.
Currently, it is not economically feasible to use ammonia as a fuel to decarbonize a TSHD. So, not with an ICE or SOFC. However, when green ammonia is used in combination with a SOFC, then a TSHD can be fully decarbonized. In order to make ammonia an economically feasible option for a TSHD, the price of MGO and carbon has to increase, or the price of the SOFC and ammonia (grey and green) has to decrease significantly.
Currently it is unclear if the carbon tax in the future applies to tank-to-wake (TTW) or well-to-wake (WTW) emissions. If the WTW emissions are taxed, then grey ammonia is never a better choice than MGO in terms of cost. Which is also the case when considering the CO2 equivalent emissions.
To conclude, it is currently not economically feasible to decarbonize a TSHD using ammonia as a fuel based on the cost per dredged material [€/m^3]. The limited transient load capabilities of drive train configurations on ammonia, need a battery or MGO to cope with the transient load of a TSHD. Future progress in the technology or developments in the reduction of transient loads could make ammonia as a fuel for a TSHD a better option. Finally, future developments in the price of: carbon, ammonia and MGO can make it economically feasible to decarbonize a TSHD.
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Ammonia needs to be handled, stored and consumed taking into account safety precautions to have a safe operable ship. Additionally, ammonia has poor combustion characteristics, and therefore a promoter such as hydrogen (7-11%) or MGO (40-60%) is necessary to initiate the combustion. Additionally, internal combustion engines (ICE) using ammonia as a fuel are expected to have a low transient load capability. Therefore, if there is no MGO present, the dynamic loading capability of the ICE with the load variation of the dredging process is a challenge. The same challenge applies for a Solid oxide fuel cell (SOFC), where the SOFC does hardly have transient load capabilities.
A TSHD currently has an ICE capable of dynamic loading, and the main reasons for this transient load is the change in propulsion power, which is dependent on the friction of the draghead and the sailing speed of the vessel. Furthermore, a sudden change in mixture density in the dredging tube during dredging will result in a sudden transient load. To cope with these transient loads, the energy supply on board of a TSHD must have transient load capabilities.
A fuel consumption model has been developed to compare five drive train configurations for the dredging project Kustlijnzorg with an operational profile of 30 days with respect to the original drivetrain. The total power demand [kW] and the transient load [kW/s] was included on a boolean way in this model. When the power demand or the transient load was too high then the model would stop. By means of this model, the main particulars of the engines, fuel cells and batteries regarding power and energy were determined. The output of this model was the amount of fuel consumed during 30 days. This fuel consumption model was validated with another project.
The Construction Industry Research and Information Association (CIRIA) has developed a method to valuate a TSHD. With this CIRIA methods, the value of a conventional TSHD is determined and compared with the value of the ammonia driven configurations. The value of a new vessel that operates on ammonia can be estimated with the help of a sustainability factor. It is found that the weekly cost of the vessel is mainly dependent on; the value of the vessel, which is dependent on the installed power and cost of technology, the fuel consumption, the cost of fuel and the carbon tax.
Currently, it is not economically feasible to use ammonia as a fuel to decarbonize a TSHD. So, not with an ICE or SOFC. However, when green ammonia is used in combination with a SOFC, then a TSHD can be fully decarbonized. In order to make ammonia an economically feasible option for a TSHD, the price of MGO and carbon has to increase, or the price of the SOFC and ammonia (grey and green) has to decrease significantly.
Currently it is unclear if the carbon tax in the future applies to tank-to-wake (TTW) or well-to-wake (WTW) emissions. If the WTW emissions are taxed, then grey ammonia is never a better choice than MGO in terms of cost. Which is also the case when considering the CO2 equivalent emissions.
To conclude, it is currently not economically feasible to decarbonize a TSHD using ammonia as a fuel based on the cost per dredged material [€/m^3]. The limited transient load capabilities of drive train configurations on ammonia, need a battery or MGO to cope with the transient load of a TSHD. Future progress in the technology or developments in the reduction of transient loads could make ammonia as a fuel for a TSHD a better option. Finally, future developments in the price of: carbon, ammonia and MGO can make it economically feasible to decarbonize a TSHD.
Methanol Drive
A methanol-fuelled Solid oxide fuel cell - internal combustion engine combined cycle for maritime applications
This work presents an in MATLAB & Simulink constructed first principles based model of a methanol fuelled SOFC-ICE combined cycle. The zero-dimensional SOFC model consists of a temperature controlled methanator which maintains an external reforming ratio of 0.5; a cell mass balance; a cell energy balance, and an electrochemical model. The ICE model core consists of a turbocharged five-state Seiliger cycle. It simulates Wärtsilä 12V31DF fuelled with methanol and dehydrated hydrogen-rich anode of gas (AOG). The SOFC efficiency and its separate losses are evaluated for different temperatures, current densities, fuel utilisation factors UF and steam-to-fuel ratio’s in combined cycle operations. Additionally, the standalone SOFC performance, without the use of waste heat from the ICE and disuse of residual fuel in the AOG, is evaluated, but only for the nominal condition. The ICE efficiency and losses are evaluated for a power range between 1% and 100%. By varying the ammount of cells, the following power splits PSOFC/PICE have been evaluated: 0/100 25/75; 50/50; 75/25 and 100/0. The combined cycle performance is evaluated for different temperatures and current densities.
This study found that while varying the steam-to-fuel ratio and fuel utilisation factor (UF) have minimal impact on the electrical efficiency of the SOFC in combined cycle operations, temperature and current density have a significant effect on the efficiency of the SOFC. For a steam-to-fuel ratio of 1:1, a UF of 0.8, a current density of 5000 A · m−2 and a mean cell temperature of 1073K an efficiency of 58.6% was obtained. The standalone SOFC, or 100/0 power split, obtained an efficiency of 48.4%. The stand-alone ICE genset, or 0/100 power split, operates at a nominal efficiency of 42.3%. When the ICE is used in a direct drive configuration, it corresponds to an efficiency of 43.6%. The combined cycle obtained efficiencies of 45.4%, 49.1% and 53.4% for 25/75, 50/50 and 75/25 power splits, respectively. These results are compared to the results of a similar study investigating an ammonia-fuelled SOFCICE combined cycle for maritime applications, which reported efficiencies of 47%, 50% and 52% for 25/75, 50/50 and 75/25 power splits, respectively, under similar operating conditions.
The efficiency gain of the methanol-fuelled 75/25 configuration compared to the direct drive is limited. This raises the questions about whether the added complexity of introducing an SOFC is justified for the limited efficiency gain. The highest efficiency was obtained with the methanol-fuelled 75/25 power split, but due to the large proportion of SOFC power, it is less tolerant to dynamics in the load, making it questionable whether it can fully meet the dynamic power demand of a ship. Therefore, the 50/50 power split configuration is expected to be the most viable option in terms of both technological feasibility and efficiency gain. A change in the power split to 100/0 results in a decrease in system efficiency due to the lack of waste heat from the ICE and the inability to utilise residual fuel in the exhaust. When considering efficiency, the values for the ammonia fuelled and methanol fuelled plant are similar.
The 50/50 powersplit configuration is 5.6 percentpoints more efficient than the methanol fuelled direct drive ICE and 1.2 percentpoints more efficient than the methanol-fuelled standalone SOFC. This clearly shows the synergistic benefits of combining a methanol-fuelled SOFC with an ICE. However, when compared to the ammonia fuelled combined cycle with 50/50 power split, it is 0.9 percentpoints less efficient. Nevertheless, it is important to exercise caution when drawing further conclusions from this last figure as the model has been constructed at a system level and no thorough uncertainty analysis has been conducted. Furthermore, the requirements regarding the power and energy density are strongly dependent on the type of ship and its operational profile. Therefore, future research should include the implementation of dynamic load capabilities in the model to evaluate its technological feasibility and overall net efficiency gain in various operational profiles of ships. Also, further research is required on the methanol-fuelled ICE cylinder process and the heat integration of the combined cycle.
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This work presents an in MATLAB & Simulink constructed first principles based model of a methanol fuelled SOFC-ICE combined cycle. The zero-dimensional SOFC model consists of a temperature controlled methanator which maintains an external reforming ratio of 0.5; a cell mass balance; a cell energy balance, and an electrochemical model. The ICE model core consists of a turbocharged five-state Seiliger cycle. It simulates Wärtsilä 12V31DF fuelled with methanol and dehydrated hydrogen-rich anode of gas (AOG). The SOFC efficiency and its separate losses are evaluated for different temperatures, current densities, fuel utilisation factors UF and steam-to-fuel ratio’s in combined cycle operations. Additionally, the standalone SOFC performance, without the use of waste heat from the ICE and disuse of residual fuel in the AOG, is evaluated, but only for the nominal condition. The ICE efficiency and losses are evaluated for a power range between 1% and 100%. By varying the ammount of cells, the following power splits PSOFC/PICE have been evaluated: 0/100 25/75; 50/50; 75/25 and 100/0. The combined cycle performance is evaluated for different temperatures and current densities.
This study found that while varying the steam-to-fuel ratio and fuel utilisation factor (UF) have minimal impact on the electrical efficiency of the SOFC in combined cycle operations, temperature and current density have a significant effect on the efficiency of the SOFC. For a steam-to-fuel ratio of 1:1, a UF of 0.8, a current density of 5000 A · m−2 and a mean cell temperature of 1073K an efficiency of 58.6% was obtained. The standalone SOFC, or 100/0 power split, obtained an efficiency of 48.4%. The stand-alone ICE genset, or 0/100 power split, operates at a nominal efficiency of 42.3%. When the ICE is used in a direct drive configuration, it corresponds to an efficiency of 43.6%. The combined cycle obtained efficiencies of 45.4%, 49.1% and 53.4% for 25/75, 50/50 and 75/25 power splits, respectively. These results are compared to the results of a similar study investigating an ammonia-fuelled SOFCICE combined cycle for maritime applications, which reported efficiencies of 47%, 50% and 52% for 25/75, 50/50 and 75/25 power splits, respectively, under similar operating conditions.
The efficiency gain of the methanol-fuelled 75/25 configuration compared to the direct drive is limited. This raises the questions about whether the added complexity of introducing an SOFC is justified for the limited efficiency gain. The highest efficiency was obtained with the methanol-fuelled 75/25 power split, but due to the large proportion of SOFC power, it is less tolerant to dynamics in the load, making it questionable whether it can fully meet the dynamic power demand of a ship. Therefore, the 50/50 power split configuration is expected to be the most viable option in terms of both technological feasibility and efficiency gain. A change in the power split to 100/0 results in a decrease in system efficiency due to the lack of waste heat from the ICE and the inability to utilise residual fuel in the exhaust. When considering efficiency, the values for the ammonia fuelled and methanol fuelled plant are similar.
The 50/50 powersplit configuration is 5.6 percentpoints more efficient than the methanol fuelled direct drive ICE and 1.2 percentpoints more efficient than the methanol-fuelled standalone SOFC. This clearly shows the synergistic benefits of combining a methanol-fuelled SOFC with an ICE. However, when compared to the ammonia fuelled combined cycle with 50/50 power split, it is 0.9 percentpoints less efficient. Nevertheless, it is important to exercise caution when drawing further conclusions from this last figure as the model has been constructed at a system level and no thorough uncertainty analysis has been conducted. Furthermore, the requirements regarding the power and energy density are strongly dependent on the type of ship and its operational profile. Therefore, future research should include the implementation of dynamic load capabilities in the model to evaluate its technological feasibility and overall net efficiency gain in various operational profiles of ships. Also, further research is required on the methanol-fuelled ICE cylinder process and the heat integration of the combined cycle.
Method - The test geometry is a NACA0012 surface-piercing hydrofoil with pressure measured using 2 rows of 15 pressure tappings. Extension pieces are used to obtain the span-wise pressure distribution while keeping the submerged span constant. The test program has three sets: all vertical runs (Set 1), high roll angle runs (Set 2), and runs with ventilation (Set 3). During the experiment, the loads are measured with force transducers on a frame that measures forces in 6 degrees of freedom. The calibration of the force transducers is performed prior to the experiment. The calibration of the pressure sensors is done first using a 9 meter water column before the experiment and during the experiment in the towing tank, extra re-calibration (stepped runs) data is collected. The collected force measurement data is processed to attain the lift and drag coefficients. The pressure measurements are translated to the pressure coefficient and placed in a matrix on the right location of the lifting surface.
Results - Based on repeated experimental runs the percentage differences are obtained on sensor and array levels. 30% of the sensors have a percentage difference of more than 10%, while the maximum difference for an entire array is 2.5%. A cross-check between the upper and lower arrays showed a percentage difference above 15% for 28% of the sensors, with a maximum difference of 1.2% at the array level. The pressure distributions at 0∘ roll angle, from Set 1, match the general pressure distribution characteristics. Comparing the 3D lift coefficient computed from the pressure measurements to that of the force data or an empirical method yields ambiguous results. The 3D lift coefficient based on the pressure measurement is within a 4% difference to Xfoil. The result of the high roll angle runs, Set 2, show the effect free-surface proximity has on the chord-wise pressure distribution. For the shallowest pressure reconstructions, close to the free-surface, the pressure distribution shows a minor peak near the leading edge after which the curve drops to near zero quickly. The operational conditions do not affect the quality of measurements. During two runs ventilation occurred, this is Set 3. The time-traces of the three forwardmost sensors show a dip prior to ventilation, with one sensor displaying an oscillating response. It is hypothesised that this is the position where ventilation is induced, but based on the results this can not be proven. All sensor response follows the same pattern when the ventilation bursts over the surface. The set-up is able to capture quick pressure changes.
Conclusion -The percentage difference is too high for too many sensors. On the array level, however, the difference is considered small enough. The results of set 1 are in good agreement with known data. The results obtained at 60∘ roll angle are concluded to be of the same quality as for 0∘ roll. The method is capable of providing results in a wide range of operational conditions. Based on the ventilation runs, no correlation to pressure reading has been found. The time-traces of the sensors near the leading edge of these runs do show fluctuations prior to ventilation. With more ventilation runs available, it is highly likely that a correlation can be established. Due to the slim data set, it is possible that the conclusions drawn will be refuted in the future when a larger data set is available. Currently, the goal has not been achieved, and it cannot be stated with certainty that the method used here to attain a full surface pressure reconstruction can be used to correlate pressure to ventilation. ...
Method - The test geometry is a NACA0012 surface-piercing hydrofoil with pressure measured using 2 rows of 15 pressure tappings. Extension pieces are used to obtain the span-wise pressure distribution while keeping the submerged span constant. The test program has three sets: all vertical runs (Set 1), high roll angle runs (Set 2), and runs with ventilation (Set 3). During the experiment, the loads are measured with force transducers on a frame that measures forces in 6 degrees of freedom. The calibration of the force transducers is performed prior to the experiment. The calibration of the pressure sensors is done first using a 9 meter water column before the experiment and during the experiment in the towing tank, extra re-calibration (stepped runs) data is collected. The collected force measurement data is processed to attain the lift and drag coefficients. The pressure measurements are translated to the pressure coefficient and placed in a matrix on the right location of the lifting surface.
Results - Based on repeated experimental runs the percentage differences are obtained on sensor and array levels. 30% of the sensors have a percentage difference of more than 10%, while the maximum difference for an entire array is 2.5%. A cross-check between the upper and lower arrays showed a percentage difference above 15% for 28% of the sensors, with a maximum difference of 1.2% at the array level. The pressure distributions at 0∘ roll angle, from Set 1, match the general pressure distribution characteristics. Comparing the 3D lift coefficient computed from the pressure measurements to that of the force data or an empirical method yields ambiguous results. The 3D lift coefficient based on the pressure measurement is within a 4% difference to Xfoil. The result of the high roll angle runs, Set 2, show the effect free-surface proximity has on the chord-wise pressure distribution. For the shallowest pressure reconstructions, close to the free-surface, the pressure distribution shows a minor peak near the leading edge after which the curve drops to near zero quickly. The operational conditions do not affect the quality of measurements. During two runs ventilation occurred, this is Set 3. The time-traces of the three forwardmost sensors show a dip prior to ventilation, with one sensor displaying an oscillating response. It is hypothesised that this is the position where ventilation is induced, but based on the results this can not be proven. All sensor response follows the same pattern when the ventilation bursts over the surface. The set-up is able to capture quick pressure changes.
Conclusion -The percentage difference is too high for too many sensors. On the array level, however, the difference is considered small enough. The results of set 1 are in good agreement with known data. The results obtained at 60∘ roll angle are concluded to be of the same quality as for 0∘ roll. The method is capable of providing results in a wide range of operational conditions. Based on the ventilation runs, no correlation to pressure reading has been found. The time-traces of the sensors near the leading edge of these runs do show fluctuations prior to ventilation. With more ventilation runs available, it is highly likely that a correlation can be established. Due to the slim data set, it is possible that the conclusions drawn will be refuted in the future when a larger data set is available. Currently, the goal has not been achieved, and it cannot be stated with certainty that the method used here to attain a full surface pressure reconstruction can be used to correlate pressure to ventilation.