Contribution of Swirl Recovery to the Induced Drag of a Propeller-Wing System – A Parametric Study

Instability of Rotating-Cone Boundary Layer in Axial Inflow: Effect of Cone Angle

The Faculty of Aerospace Engineering at Delft University of Technology

Aerodynamic Performance of an Aircraft with Aft-Fuselage Boundary-Layer-Ingestion Propulsion

Development of an experimental apparatus for flat plate drag measurements and considerations for such measurements

Sub-scale flight test model design: Developments, challenges and opportunities

Experimental Investigation of Aerodynamic Interactions of a Wing with Deployed Fowler Flap under Influence of a Propeller Slipstream

Spiral instability-modes on rotating cones in high-Reynolds number axial flow

Propeller Performance at Large Angle of Attack Applicable to Compound Helicopters

Experimental Investigation of Over-the-Wing Propeller–Boundary-Layer Interaction

Numerical Investigation of Propeller–Flap Interaction in Inclined Over-the-Wing Distributed-Propulsion Systems

The impact of skinsuit zigzag tape turbulators on speed skating performance

Aerodynamic Interaction Effects Between Propellers in Typical eVTOL Vehicle Configurations

Aerodynamic Performance of an Aircraft with Aft-Fuselage Boundary Layer Ingestion Propulsion

Boundary layer instability over a rotating slender cone under non-axial inflow

Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight

Power balance analysis experiments on an axisymmetric fuselage with an integrated boundary-layer-ingesting fan

Aerodynamic Performance and Static Stability Characteristics of Aircraft with Tail-Mounted Propellers

Breakdown of aerodynamic interactions for the lateral rotors on a compound helicopter

Engineering method to estimate the blade loading of propellers in nonuniform flow