Experimentally determined local flow properties and drag coefficients for a family of blunt bodies at Mach numbers from 2.49 to 4.63

Experimentally determined local flow properties and drag coefficients for family of blunt bodies at Mach numbers from 2.49 to 4.63

[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 .