top of page

Aerodynamics

Scanning Lagrangian Particle Tracking To Measure 3D Large Scale Aerodynamics Of Quadcopter Flight

Scanning Lagrangian Particle Tracking To Measure 3D Large Scale Aerodynamics Of Quadcopter Flight

Daniel Schanz, Andreas Schröder, Johannes Bosbach, Tobias Strübing, Claus Christian Wolf, Clemens Schwarz, Alexander Heintz

German Aerospace Center (DLR), Göttingen, Germany

Aerodynamic and acoustic investigations of rotor-rotor wake interaction

Aerodynamic and acoustic investigations of rotor-rotor wake interaction

Fabrizio De Gregorio (1), Karl-Stephane Rossignol (2), Giuseppe Ceglia (1), Jianping Yin (2)

1. CIRA, Italian Aerospace Research Centre, Capua, Italy
2. DLR, German Aerospace Centre, Braunschweig, Germany

Particle Image Velocimetry Investigation Of The Aerodynamic Interaction Between Helicopter And An Aircraft Carrier

Particle Image Velocimetry Investigation Of The Aerodynamic Interaction Between Helicopter And An Aircraft Carrier

Rafael Bardera, Juan Carlos Matias, Estela Barroso

Nanjing University of Science and Technology, Nanjing, China

An Experimental Investigation Of µUAV Rotor Wingtip Vortices Through High Spatial Resolution PIV

An Experimental Investigation Of µUAV Rotor Wingtip Vortices Through High Spatial Resolution PIV

Giosuè Longobardo (1), Tommaso Astarita (1), Fabrizio De Gregorio (2)

1. Università degli Studi di Napoli, Napoli, Italy
2. Centro Italiano Ricerche Aerospaziali, Capua, Italy

An Appraisal Of Large-Scale Particle Tracking With Uncrewed Aerial Vehicles

An Appraisal Of Large-Scale Particle Tracking With Uncrewed Aerial Vehicles

Robin Leister (1), David E. Rival (2)

1. Institute of Fluid Mechanics - Karlsruhe Institute of Technology, Karlsruhe, Germany
2. Institute of Fluid Mechanics - Technische Universität Braunschweig, Braunschweig, Germany

Effects Of Wing Elasticity On Tip Vortex: 3D Deformation And 2D3C Flow Field Measurements

Effects Of Wing Elasticity On Tip Vortex: 3D Deformation And 2D3C Flow Field Measurements

Qinfeng Guo, Jinjun Wang

Beijing University of Aeronautics and Astronautics, Beijing, China

Spatial And Temporal Modes On A Generic Tandem Configuration In Transonic Shock Buffet

Spatial And Temporal Modes On A Generic Tandem Configuration In Transonic Shock Buffet

Christopher Julian Schauerte, Anne-Marie Schreyer

Institute of Aerodynamics RWTH Aachen University, Aachen, Germany

Application Of Temperature-Sensitive Paint For Transition Detection On An NLF Forward-Swept Wing Under Harmonic Pitch Oscillation At Flight-Relevant Mach And Reynolds Numbers

Application Of Temperature-Sensitive Paint For Transition Detection On An NLF Forward-Swept Wing Under Harmonic Pitch Oscillation At Flight-Relevant Mach And Reynolds Numbers

Nils Paul Van Hinsberg, Ulrich Henne, Christian Klein

Institute of Aerodynamics and Flow Technology - German Aerospace Center, Goettingen, Germany

Flow Development Over An SD7003 Airfoil At Different Accelerations From Rest

Flow Development Over An SD7003 Airfoil At Different Accelerations From Rest

Christian J. Kähler, Wolfgang Dierl, Rainer Hain

University of the Bundeswehr Munich, Neubiberg, Germany

bottom of page