Development of the TAU-Code for aerospace applications D Schwamborn, A Gardner, H von Geyr, A Krumbein, H Lüdeke, ... | 104 | 2008 |
Improved Two-Dimensional Dynamic Stall Prediction with Structured and Hybrid Numerical Methods K Richter, A Le Pape, T Knopp, M Costes, V Gleize, AD Gardner Journal of the American Helicopter Society 56 (4), 1-12, 2011 | 90 | 2011 |
Analysis of dynamic stall using dynamic mode decomposition technique S Mariappan, AD Gardner, K Richter, M Raffel AIAA journal 52 (11), 2427-2439, 2014 | 83 | 2014 |
Upstream porthole injection in a 2-D scramjet model AD Gardner, A Paull, TJ McIntyre Shock Waves 11 (5), 369-375, 2002 | 77 | 2002 |
Ground testing of the HyShot supersonic combustion flight experiment in HEG and comparison with flight data A Gardner, J Steelant, A Paull, K Hannemann 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 3345, 2004 | 67 | 2004 |
Investigation of three-dimensional dynamic stall on an airfoil using fast-response pressure-sensitive paint AD Gardner, C Klein, WE Sachs, U Henne, H Mai, K Richter Experiments in fluids 55, 1-14, 2014 | 51 | 2014 |
Experimental study of secondary vortex structures in a rotor wake CC Wolf, C Schwarz, K Kaufmann, AD Gardner, D Michaelis, J Bosbach, ... Experiments in Fluids 60 (11), 175, 2019 | 46 | 2019 |
Experimental investigation of unsteady transition on a pitching rotor blade airfoil K Richter, S Koch, AD Gardner, H Mai, A Klein, CH Rohardt Journal of the American Helicopter Society 59 (1), 1-12, 2014 | 42 | 2014 |
Dynamic stall simulations on a pitching finite wing K Kaufmann, CB Merz, AD Gardner Journal of Aircraft 54 (4), 1303-1316, 2017 | 41 | 2017 |
Boundary-layer transition on a rotor blade measured by temperature-sensitive paint, thermal imaging and image derotation W Lang, AD Gardner, S Mariappan, C Klein, M Raffel Experiments in Fluids 56, 1-14, 2015 | 41 | 2015 |
Experimental investigation of dynamic stall performance for the EDI-M109 and EDI-M112 airfoils AD Gardner, K Richter, H Mai, ARM Altmikus, A Klein, CH Rohardt Journal of the American Helicopter Society 58 (1), 1-13, 2013 | 41 | 2013 |
Numerical investigation of three-dimensional static and dynamic stall on a finite wing K Kaufmann, M Costes, F Richez, AD Gardner, AL Pape Journal of the American Helicopter Society 60 (3), 1-12, 2015 | 36 | 2015 |
Review of measurement techniques for unsteady helicopter rotor flows AD Gardner, CC Wolf, M Raffel Progress in Aerospace Sciences 111, 100566, 2019 | 35 | 2019 |
Numerical investigation of air jets for dynamic stall control on the OA209 airfoil AD Gardner, K Richter, H Rosemann CEAS Aeronautical Journal 1 (1), 69-82, 2011 | 34 | 2011 |
A novel experiment to understand the dynamic stall phenomenon in rotor axial flight T Schwermer, AD Gardner, M Raffel Journal of the American Helicopter Society 64 (1), 1-11, 2019 | 33* | 2019 |
A new method of dynamic and static stall detection using infrared thermography AD Gardner, CC Wolf, M Raffel Experiments in Fluids 57 (9), 149, 2016 | 33 | 2016 |
Detection of unsteady boundary layer transition using three experimental methods K Richter, CC Wolf, A Gardner, CB Merz 54th AIAA aerospace sciences meeting, 1072, 2016 | 32 | 2016 |
Boundary layer transition determination for periodic and static flows using phase-averaged pressure data AD Gardner, K Richter Experiments in Fluids 56, 1-13, 2015 | 32 | 2015 |
Experimental investigation of air jets for the control of compressible dynamic stall AD Gardner, K Richter, H Mai, D Neuhaus Journal of the American Helicopter Society 58 (4), 1-14, 2013 | 32* | 2013 |
On the effect of rotational forces on rotor blade boundary-layer transition A Weiss, AD Gardner, T Schwermer, C Klein, M Raffel AIAA Journal 57 (1), 252-266, 2019 | 31 | 2019 |