Experimentally determined local flow properties and drag coefficients for a family of blunt bodies at Mach numbers from 2.49 to 4.63
暂无分享,去创建一个
[1] Milton D. VanDyke,et al. Supersonic Flow past a Family of Blunt Axisymmetric Bodies , 1959 .
[2] A. Charters,et al. The Aerodynamic Performance of Small Spheres from Subsonic to High Supersonic Velocities , 1945 .
[3] J. R. Stalder,et al. Heat transfer from a hemisphere-cylinder equipped with flow-separation spikes , 1954 .
[4] A. J. Hodges. The Drag Coefficient of Very High Velocity Spheres , 1957 .
[5] H. Serbin. Supersonic Flow Around Blunt Bodies , 1958 .
[6] M. Inouye,et al. Blunt body solutions for spheres and ellipsoids in equilibrium gas mixtures , 1965 .
[7] P. E. Everhart,et al. An experimental study of the pressure and heat-transfer distribution on a 70 deg sweep slab delta wing in hypersonic flow , 1963 .
[8] S. Traugott. An Approximate Solution of the Direct Supersonic Blunt-Body Problem for Arbitrary Axisymmetric Shapes , 1960 .
[9] Morton Cooper,et al. Measurements of Local Heat Transfer and Pressure on Six 2-Inch-Diameter Blunt Bodies at a Mach Number of 4.95 and at Reynolds Numbers Per Foot up to 81 x 10(exp 6) , 1959 .
[10] Robert E. Oliver. Part I. The effect of a simple throat distortion on the downstream flow in a hypersonic wind tunnel nozzle. Part II. An experimental investigation of flow over simple blunt bodies at a nominal Mach number of 5.8 , 1957 .
[11] J. C. Boison. An Experimental Investigation of Blunt Body Stagnation Point Velocity Gradient , 1959 .
[12] R. Swigart. A THEORY OF ASYMMETRIC HYPERSONIC BLUNT-BODY FLOWS , 1963 .
[13] J. C. Dunavant,et al. Effect of roughness on heat transfer to hemisphere cylinders at Mach numbers 10.4 and 11.4 , 1967 .
[14] E. V. Zoby,et al. Effects of Corner Radius on Stagnation-point Velocity Gradients on Blunt Axisymmetric Bodies , 1966 .