Vortical flow prediction for the design of a wind tunnel experiment with a pitching lambda wing
Author:
Publisher
Springer Science and Business Media LLC
Subject
Aerospace Engineering,Transportation
Link
http://link.springer.com/content/pdf/10.1007/s13272-014-0120-5.pdf
Reference18 articles.
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3. Voss, G., Cumnuantip, S., Neumann, J.: A steady aeroelastic analysis of an unmanned combat aircraft, vehicle conceptual design, 29th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii, AIAA 2011-3020 (2011) doi: 10.2514/6.2011-3020
4. Schuette, A., Hummel, D., Hitzel, S.M.: Numerical and experimental analyses of the vortical flow around the SACCON configuration, Fluid Dynamics and Co-located Conferences, Chicago, Illinois, AIAA, 2010-4690 (2010) doi: 10.2514/6.2010-4690
5. Gerhold, T., Friedrich, O., Evans, J.: Calculations of Complex Three-dimensional Configurations Employing the DLR-TAU-Code, Reno, Nevada, AIAA 97-0167 (1997) doi: 10.2514/6.1997-167
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1. Numerical Modelling of a Wind Tunnel Experiment to Investigate Vortex-Dominated Flow at Medium and High Angles of Attack;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2021
2. Unsteady surface pressures measured at a pitching Lambda wing with vortex dominated flow and transonic effects;CEAS Aeronautical Journal;2018-03-09
3. Motion-Induced Unsteady Aerodynamic Loads with Development of Vortical Flow;Journal of Aircraft;2018-01
4. Motion induced unsteady aerodynamic loads with development of vortical flow;55th AIAA Aerospace Sciences Meeting;2017-01-05
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