The Flow over a Flat Plate with a Small Angle of Attack at Mach Number 1
暂无分享,去创建一个
[1] G. Guderley,et al. Two-Dimensional Unsymmetric Flow Patterns at Mach Number 1 , 1953 .
[2] David T. Barish. Asymptotic Forms of Shock Waves in Flows over Symmetrical Bodies at Mach 1 , 1953 .
[3] G. Maslach. A Precision Differential Manometer , 1952 .
[4] S. Bogdonoff. A Preliminary Study of Reynolds Number Effects on Base Pressure at M = 2.95* , 1952 .
[5] Luigi Crocco,et al. A Mixing Theory for the Interaction between Dissipative Flows and Nearly-Isentropic Streams , 1952 .
[6] Dean R Chapman,et al. An analysis of base pressure at supersonic velocities and comparison with experiment , 1951 .
[7] G. Guderley,et al. THE FLOW OVER A WEDGE PROFILE AT MACH NUMBER ONE , 1950 .
[8] Edward W Perkins,et al. Experimental investigation of the effects of support interference on the drag of bodies of revolution at a Mach number of 1.5 , 1948 .
[9] Rudolph E. Langer,et al. On the asymptotic solutions of ordinary differential equations, with an application to the Bessel functions of large order , 1931 .