[1] Keener E R, Chapman G T. Similarity in vortex asymmetric over slender bodies and wings[J]. AIAA J, 1977, 12(15):1370-1372.
[2] Ericsson L E. Sources of high alpha vortex asymmetry at zero sideslip[J]. Journal of Aircraft, 1992, 29(6):1086-1090.
[3] Peake D J, Tobak M. Three dimensional interactions and vortical flow with emphasis on high speeds[R]. AGARD-AG-252, 1980.
[4] Nishioka M, Sato H. Mechanism of determination of the shedding frequency of vortices behind a cylinder at low Reynolds numbers[J]. Journal of Fluid Mechanics, 1978, 89(1):49-60.
[5] LI Guo-hui, DENG Xue-ying. Topological structure evolution and stability of the cross flow patternaround a slender[J]. Journal of BUAA, 2001, 27(6):674-676. (in Chinese).
[6] Maskell E C. Flow separation in three dimensions[R]. RAE Aero Rept, 2565, 1955.
[7] LU Qi-shao. Qualitative Method of Differential Equation and Bifurcation [M]. Beijing:BUAA Press, 1989. (in Chinese).
[8] Lowson M V, Ponton A J. Symmetry breaking in vortex flows on conical bodies[J]. AIAA J, 1992, 30(6):1341-1352.
[9] Werl? H. La Tunnel hg drodgnanique au service de la recherche aerospatiale[R]. ONERA Publication, No 156, 1974.
[10] CHEN Xue-rui, DENG Xue-ying, WANG Yan-kui, et al. Influence of nose perturbations on behaviors of asymmetric vortices over slender body[J]. Acta Mechanica Sinica, 2002, 18(6):581-593.
[11] Luo S C, Lim T T, Lua K B, et al. Flowfield around ogive/elliptic-tip cylinder at high angle of attack[J]. AIAA J, 1998, 36(10):1778-1787.
[12] Bernhardt J E, Williams D R. Proportional control of asymmetric forebody vortices[J]. AIAA J, 1998, 36(11):2087-2093.
[13] Bridges D H, Homung H G. Elliptic tip effects on the vortex wake of an axisymmetric body at incidence[J]. AIAA J, 1994, 32(7):1437-1445.
[14] Wardlow A B Jr, Yanta W J. Asymmetric flowfield development on a slender body at high incidence[J]. AIAA J, 1984, 22(2):233-245. |