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DeHNSSo
DeHNSSo: The Delft Harmonic Navier-Stokes Solver for Nonlinear Stability Problems with Complex Geometric Features
Non-Modal Growth Induced by Discrete Roughness Elements in a Swept Wing Boundary Layer
Non-Modal Growth Induced by Discrete Roughness Elements in a Swept Wing Boundary Layer: Modelling and Diagnostics
Influence of a forward-facing step on crossflow instability and transition
Influence of a forward-facing step on crossflow instability and transition: An experimental study in a swept wing boundary-layer
Boundary-layer instability on rotating cones
Boundary-layer instability on rotating cones: An experiment-based exploration
Influence of a Wall-Embedded Phononic Crystal on Tollmien-Schlichting Waves
Influence of a Wall-Embedded Phononic Crystal on Tollmien-Schlichting Waves
Cross-Flow Instability Control through Base-Flow Modification using AC-DBD Plasma Actuators
Cross-Flow Instability Control through Base-Flow Modification using AC-DBD Plasma Actuators: An Experimental Investigation
Application of Acoustic Metamaterials in Boundary Layer Instability Control
Application of Acoustic Metamaterials in Boundary Layer Instability Control
Advanced Infrared Thermography Data Analysis for Unsteady Boundary Layer Transition Detection
Advanced Infrared Thermography Data Analysis for Unsteady Boundary Layer Transition Detection
Unsteady Boundary Layer Transition Measurements with Infrared Thermography
Unsteady Boundary Layer Transition Measurements with Infrared Thermography: Development of Improved Measurement Schemes
Cross-Flow Instability
Cross-Flow Instability: Flow diagnostics and control of swept wing boundary layers
Drag reduction by applying speedstrips on rowing oars
Drag reduction by applying speedstrips on rowing oars
Flow visualization of swept wing boundary layer transition
Flow visualization of swept wing boundary layer transition
Experimental investigation of re-entry aerodynamic phenomena - Development of non-intrusive ?ow diagnostics in a Ludwieg tube
Experimental investigation of re-entry aerodynamic phenomena - Development of non-intrusive ?ow diagnostics in a Ludwieg tube
Potential applications of laser anemometry for in-flight measurements
Potential applications of laser anemometry for in-flight measurements
Boudary layer measurements on a two-dimensional wing with flap
Boudary layer measurements on a two-dimensional wing with flap
Reynolds number effects on pressure and normal force distributions along conically pointed circular cylinder at free-stream mach number of 2.3
Reynolds number effects on pressure and normal force distributions along conically pointed circular cylinder at free-stream mach number of 2.3
Contribution à la transition dans la couche limite
Contribution à la transition dans la couche limite
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