[1] |
Katz J.Wing/vortex interactions and wing rock[J].Progress in Aerospace Sciences, 1999, 35:727-750.
|
[2] |
Quast T, Nelson R C, Fisher D F.A study of high alpha dynamics and flow visualization for a 2.5% model of the F-18 HARV undergoing wing rock[J].AIAA, 1991, 3267-CP:524-533.
|
[3] |
Klein V, Noderer K D.Aerodynamic parameters of the X-31 drop model estimated from flight data at high angles of attack[J].AIAA, 1992, 4357:174-181.
|
[4] |
Brandon J M, Nguyen L T.Experimental study of effects of forebody geometry on high angle of attack stability[J].Journal of Aircraft, 1988, 25(7):591-597.
|
[5] |
Ericsson L E.Wing rock generated by forebody vortices[J].Journal of Aircraft, 1989, 26(2):110-116.
|
[6] |
Ericsson L E.Further analysis of wing rock generated by forebody vortices[J].Journal of Aircraft, 1989, 26(12):1098-1104.
|
[7] |
马宝峰.前体涡诱导机翼摇滚的实验研究[D].北京:北京航空航天大学, 2007. Ma B F.Experimental investigation of roll oscillation induced by forebody vortex[D].Beijing:Beihang University, 2007(in Chinese).
|
[8] |
Wang B, Deng X Y, Ma B F, et al.Effect of tip perturbation and wing locations on rolling oscillation induced by forebody vortices[J].Acta Mechanica Sinica, 2010, 26(5):787-791.
|
[9] |
荣臻.前体涡诱导机翼摇滚的流动特性及机理研究[D].北京:北京航空航天大学, 2009. Rong Z.An experimental investigation on flow characteristics and mechanism of wing rock induced by forebody vortex[D].Beijing:Beihang University, 2009(in Chinese).
|
[10] |
Dexter P C, Hunt B L.The effect of roll angle on the flow over a slender body of revolution at high angles of attack[J].AIAA, 1981, 0358:1-13.
|
[11] |
Zilliac G G, Degani D, Tobak M.Asymmetric vortices on a slender body of revolution[J].AIAA, 1991, 29(5):667-675.
|
[12] |
Dexter P C.A study of asymmetric flow over slender bodies at high angles of attack in a low turbulence environment[J].AIAA, 1984, 0505:1-11.
|
[13] |
Moskovitz C A, Raleigh N C, Hall R M, et al.Effects of surface perturbations on the asymmetric vortex flow over a slender body[J].AIAA, 1988, 0483:1-10.
|
[14] |
Moskovitz C A, Hall R M, Dejarnette F R.Effects of nose bluntness, roughness and surface perturbations on the asymmetric flow past slender bodies at iarge angles of attack[J].AIAA, 1989, 2236-CP:720-732.
|
[15] |
Chen X R, Deng X Y, Wang Y K, et al.Influence of nose perturbations on behaviors of asymmetric vortices over slender body[J].Acta Mechanica Sinica, 2002, 18(6):581-593.
|
[16] |
Hunt B L.Asymmetric vortex forces and wakes on slender bodies[J].AIAA, 1982, 1336:1-41.
|
[17] |
Lamont P J.Pressures around an inclined ogive cylinder with laminar, transitional, or turbulent separation[J].AIAA, 1982, 20(11):1492-1499.
|
[18] |
Li Y P, Ge F Y, Lan C E.Estimation of aircraft models in cobra maneuver through dynamic inversion[J].AIAA, 1994, 3494-CP:322-332.
|
[19] |
Alcorn C W, Croom M A, Francis M S, et al.The X-31 aircraft:Advances in aircraft agility and performance[J].Progress in Aerospace Sciences, 1996, 32:377-413.
|
[20] |
田伟.细长旋成体及融合体型机身大迎角背涡流动特性研究[D].北京:北京航空航天大学, 2010. Tian W.Study on behaviors of leeward vortices over slender body and chined fuselage at high angle of attack[D].Beijing:Beihang University, 2010(in Chinese).
|
[21] |
曹博超.风洞动态测压技术及其在机翼摇滚运动研究中的应用[D].北京:北京航空航天大学, 2008. Cao B C.Dynamic pressure measurement technology in the wind tunnel and its application in the investigation of wing-rock phenomenon[D].Beijing:Beihang University, 2008(in Chinese).
|
[22] |
王刚,邓学蓥,王延奎,等.亚临界雷诺数细长体绕流流态随迎角的变化和分区[J].流体力学实验与测量, 2003, 17(2):19-26. Wang G, Deng X Y, Wang Y K, et al.Zonal study of flow patterns around an ogive-cylinder at subcritical reynolds numbers[J].Experiments and Measurements in Fluid Mechanics, 2003, 17(2):19-26(in Chinese).
|
[23] |
Lamont P J, Hunt B L.Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic stream[J].J Fluid Mech, 1976, 76(3):519-559.
|
[24] |
Keener E R, Chapman L C, Talegbani J.Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and mach numbers from 0.1 to 0.7[J].NASA, 1977, TM, X-3437:1-109.
|
[25] |
Ericsson L E, Reding J P.Aerodynamic effects of asymmetric vortex shedding from slender bodies[J].AIAA, 1985, 1797:222-256.
|
[26] |
Lamont P J.Pressures around an inclined ogive cylinder with laminar, transitional, or turbulent[J].AIAA, 1980, 1556R:1-10.
|