Nonlinear Response of Vortex Breakdown over a Pitching Delta Wing
Author:
Affiliation:
1. University of Cincinnati, Cincinnati, Ohio 45221-0072
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2481
Reference17 articles.
1. Some Experiments with Vortex Breakdown
2. On fluctuations of vortex breakdown location
3. Further experiments on fluctuations of vortex breakdown location
4. Self-excited oscillations of vortex breakdown location over delta wings
5. Unsteady flow phenomena over delta wings at high angle of attack
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1. Effects of Reduced Frequency on the Behaviors of Burst Point Around a Pitching Double Delta Wing;Fluid-Structure-Sound Interactions and Control;2018-05-15
2. Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods;Journal of Visualized Experiments;2018-04-23
3. Effect of pitch down motion on the vortex reformation over fighter aircraft;Aerospace Science and Technology;2018-02
4. Dynamic response of vortex breakdown flows to a pitching double-delta wing;Aerospace Science and Technology;2018-01
5. AN EVALUATION OF TURBULENCE MODEL FOR VORTEX BREAKDOWN DETECTION OVER DELTA WING;ARCH MECH ENG;2018
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