Transformation of flow structure on a delta wing of moderate sweep angle during pitch-up maneuver
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Published:2012-08
Issue:
Volume:33
Page:59-69
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ISSN:0889-9746
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Container-title:Journal of Fluids and Structures
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language:en
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Short-container-title:Journal of Fluids and Structures
Subject
Mechanical Engineering
Reference16 articles.
1. Compact difference scheme applied to the simulation of a low sweep delta wing flow;Gordnier;AIAA Journal,2005
2. Effect of pitch rate on near-surface topology on a delta wing;Goruney;AIAA Journal,2010
3. Review of unsteady vortex flows over slender delta wings;Gursul;Journal of Aircraft,2005
4. Instantaneous three-dimensional vorticity measurements in vortical flow over a delta wing;Honkan;AIAA Journal,1997
5. Jarrah, M.A.M., 1990. Visualization of the flow about a delta wing maneuvering in pitch to very high angle of attack, In: Miller, J.A., Telionis, D.P. (Eds.), International Symposium on Nonsteady Fluid Dynamics, ASME Fluids Engineering Division Proceedings, New York, USA, pp. 109–116.
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