Fluid Mechanism of Wing Rock for Configurations with Chine-Shaped Forebodies
暂无分享,去创建一个
[1] M Hall Robert. Impact of Fuselage Cross Section on the Stability of a Generic Fighter , 1998 .
[2] L. Ericsson. MOVING WALL EFFECTS IN UNSTEADY FLOW , 1988 .
[3] R. F. Warming,et al. An Implicit Factored Scheme for the Compressible Navier-Stokes Equations , 1977 .
[4] J. M. Brandon,et al. LOW-SPEED EXPERIMENTAL STUDY OF THE VORTEX FLOW EFFECTS OF A FIGHTER FOREBODY HAVING UNCONVENTIONAL CROSS-SECTION , 1985 .
[5] M. R. Mendenhall,et al. Review of forebody-induced wing rock , 1996 .
[6] William H. Mason,et al. A computational study on directional stability of chine-shaped forebodies at high-alpha , 1992 .
[7] Kenneth Wurtzler. Numerical analysis of a chined forebody with asymmetric strakes , 1993 .
[8] L. T. Nguyen,et al. Experimental study of effects of forebody geometry on high angle of attack static and dynamic stability , 1986 .
[9] T. Pulliam,et al. A diagonal form of an implicit approximate-factorization algorithm , 1981 .
[10] L. E. Ericsson,et al. Wing rock generated by forebody vortices , 1987 .
[11] E. Polhamus. Predictions of vortex-lift characteristics based on a leading-edge suction analogy. , 1971 .
[12] D. Whitfield. Three-dimensional unsteady Euler equation solutions using flux vector splitting , 1983 .
[13] Lars E. Ericsson,et al. THE VARIOUS SOURCES OF WING ROCK , 1988 .