论文信息 - Missile Datcom - High angle of attack capabilities - 字舞流文

Missile Datcom - High angle of attack capabilities

James Simon | William Blake | W. Blake | James M. Simon

[1] William B Baker. An Aerodynamic Coefficient Prediction Technique for Slender Bodies with Low Aspect Ratio Fins at Mach Numbers from 0.6 to 3.0 and Angles of Attack from 0 to 180 Degrees , 1978 .

[2] William B. Blake. Missile Datcom: User's Manual - 1997 FORTRAN 90 Revision. , 1998 .

[3] G R Gomillion. A Compilation of Static Stability and Fin Loads Data for Slender Body Missile Models With and Without Tail Fins and Wings. Volume 1 , 1976 .

[4] M. J. Hemsch,et al. Equivalent angle-of-attack method for estimating nonlinear aerodynamics of missile fins , 1983 .

[5] H. Julian Allen,et al. A study of effects of viscosity on flow over slender inclined bodies of revolution , 1951 .

[6] L. H. Jorgensen. Prediction of static aerodynamic characteristics for slender bodies alone and with lifting surfaces to very high angles of attack , 1976 .