Forebody Flow During the Wing Rock Over Low Swept Wing/Body Configuration in High Rate Pitching-up
Author:
Publisher
Elsevier BV
Subject
Applied Mathematics
Reference12 articles.
1. Joseph Katz. Wing/Vortex Interactions and Wing Rock [J]. Progress in Aerospace Sciences, 1999, 35(7): 727-750.
2. Brandon, J.M., and Nguyen, L.T., “Experimental Study of Effects of Forebody Geometry on High Angle of Attack Stability,” Journal of Aircraft, Vol. 25, July 1988, pp. 591-597.
3. Ericsson, L.E., “Wing Rock Generated by Forebody Vortices,” Journal of Aircraft, Vol. 26, Feb. 1989, pp. 110-116.
4. Ericsson, L.E., “Further Analysis of Wing Rock Generated by Forebody Vortices,” Journal of Aircraft, Vol. 26, Dec. 1989, pp. 1098-1104.
5. Wang, B., Deng, X.Y., Ma, B.F., et al., “Effect of Tip Perturbation and Wing Locations on Rolling Oscillation Induced by Forebody. Vortices,” ActaMech Sin, 26, 2010, pp.787-791.
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