Vortex breakdown over delta wings in unsteady free stream

Author:

GURSUL ISMET1,HO CHIH-MING2

Affiliation:

1. Cincinnati Univ., OH

2. California Univ., Los Angeles

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. "Sur I'eclatement des tourbillons

2. dP I!)6O, pp. 23-30. Figure 13: Variation of instantaneous pressure on a thin 2-D airfoil in unsteady free stream jk=O.'):l. 1.Lambourne, N.C. and Bryer, D.W. "The bursting R=0.42). of leading edge vortices-Some observations and

3. Idiscussion of the phenomenon", Aeronautical Research Council, R. & M. No. 3282, 1962.

4. Lift Force of Delta Wings

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1. A Low-Order Nonlinear State-Space Model for Delta Wing Leading Edge Vortices;AIAA Guidance, Navigation, and Control Conference and Exhibit;2006-06-15

2. Review of Unsteady Vortex Flows over Slender Delta Wings;Journal of Aircraft;2005-03

3. Trailing-edge jet control of leading-edge vortices of a delta wing;AIAA Journal;1996-07

4. Numerical simulation of an oscillating wing using overset grids;14th Applied Aerodynamics Conference;1996-06-17

5. Computation of vortex breakdown on a rolling delta wing;Journal of Aircraft;1995-05

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