Citation: | LI Guo-hui, DENG Xue-ying. Stability of the Crossflow Pattern Around a Slender and Influence of Disturbance[J]. Applied Mathematics and Mechanics, 2004, 25(12): 1239-1248. |
[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. doi: 10.2514/3.56864
|
[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. doi: 10.1017/S0022112078002451
|
[5] |
李国辉,邓学蓥.细长体截面流态拓扑结构演化及其稳定性分析[J].北京航空航天大学学报,2001,27(6):674—676.
|
[6] |
Maskell E C.Flow separation in three dimensions[R]. RAE Aero Rept,2565,1955.
|
[7] |
陆启韶.常微分方程的定性方法和分叉[M].北京:北京航空航天大学出版社,1989.
|
[8] |
Lowson M V,Ponton A J.Symmetry breaking in vortex flows on conical bodies[J].AIAA J,1992,30(6):1341—1352.
|
[9] |
Werlé 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. doi: 10.1007/BF02487960
|
[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. doi: 10.2514/2.286
|
[12] |
Bernhardt J E,Williams D R.Proportional control of asymmetric forebody vortices[J].AIAA J,1998,36(11):2087—2093. doi: 10.2514/2.310
|
[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. doi: 10.2514/3.12213
|
[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.
|