Determining the side force appearance and its magnitude over a slender body at high angle of attack
Author:
Publisher
Pleiades Publishing Ltd
Subject
Nuclear and High Energy Physics,Radiation
Link
https://link.springer.com/content/pdf/10.1134/S0869864321060160.pdf
Reference30 articles.
1. E.R. Keener, G.T. Chapman, and R.L. Kruse, Effects of Mach number and afterbody length on onset of asymmetric forces on bodies at zero sideslip and high angles of attack, AIAA paper, 1976, 66.
2. J.E. Fidler, Active control of asymmetric vortex effects, J. Aircraft, 1981, Vol. 18, No. 4, 267–272.
3. P.J. Lamont, Pressures around an inclined ogive cylinder with laminar, transitional, or turbulent separation, AIAA J., 1982, Vol. 20, No. 11, P. 1492–1499.
4. J. Katz and K. Ward, Development of flow structures in the Lee of an inclined body of revolution, J. Aircraft, 1989, Vol. 26, No. 3, P. 198–206.
5. G.G. Zilliac, D. Degani, and M. Tobak, Asymmetric vortices on a slender body of revolution, AIAA J., 1991, Vol. 29, No. 5, P. 667–675.
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