Anthony D. Gardner

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Markus RaffelDLR Göttingen / Leibniz Universität Hannover / PIVTEC GmbHEmail verificata su dlr.de
sathesh mariappanDepartment of Aerospace Engineering, Indian Institute of Technology KanpurEmail verificata su iitk.ac.in
Francois RichezResearch ScientistEmail verificata su onera.fr
Tobias KnoppDLR Institute for Aerodynamics and Flow TechnologyEmail verificata su dlr.de
Vincent GleizeOneraEmail verificata su onera.fr
Timothy J McIntyreThe University of QueenslandEmail verificata su uq.edu.au
Christoph DollingerEmail verificata su dollinger.name
Christoph MertensPhD Candidate, TU DelftEmail verificata su tudelft.nl
Peter JacobsReader, The University of QueenslandEmail verificata su mech.uq.edu.au
Manuel KeßlerHead of Rotorcraft & Aeroacoustics, Institute of Aerodynamics and Gas Dynamics, University ofEmail verificata su iag.uni-stuttgart.de
Marilyn J. SmithProfessor of Aerospace Engineering, Georgia Institute of TechnologyEmail verificata su ae.gatech.edu
Rohit JainAerospace Engineer, US ArmyEmail verificata su mail.mil
Daniel SchanzDeutsches Zentrum für Luft- und Raumfahrt, Dept. of Experimental MethodsEmail verificata su dlr.de
Andreas SchröderDeutsches Zentrum für Luft- und RaumfahrtEmail verificata su dlr.de
Jens NitzscheInstitute of Aeroelasticity, German Aerospace Center (DLR)Email verificata su dlr.de
Johannes LetzgusAerostack GmbHEmail verificata su airbus.com
Benjamin EwersGerman Aerospace Center (DLR)Email verificata su dlr.de
Mark PotsdamAerospace Engineer, US ArmyEmail verificata su mail.mil
Ferry SchrijerDelft University of TechnologyEmail verificata su tudelft.nl
Bas van Oudheusdenassociate professor, Delft University of TechnologyEmail verificata su tudelft.nl

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Anthony D. Gardner

DLR

Email verificata su dlr.de - Home page

dynamic stall flow control aerodynamics helicopter rotor


Titolo Ordina per citazioni Ordina per anno Ordina per titolo	Citata da Citata da	Anno
Development of the TAU-Code for aerospace applications D Schwamborn, A Gardner, H von Geyr, A Krumbein, H Lüdeke, ...	103	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	91	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	82	2014
Upstream porthole injection in a 2-D scramjet model AD Gardner, A Paull, TJ McIntyre Shock Waves 11 (5), 369-375, 2002	76	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	72	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	53	2014
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	46	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	43	2019
Dynamic stall simulations on a pitching finite wing K Kaufmann, CB Merz, AD Gardner Journal of Aircraft 54 (4), 1303-1316, 2017	40	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	40	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	40	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	37	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
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	34*	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 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
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
Analysis of differential infrared thermography for boundary layer transition detection AD Gardner, C Eder, CC Wolf, M Raffel Experiments in Fluids 58 (9), 122, 2017	31	2017

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