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A method for predicting shock shapes and pressure distributions for a wide variety of blunt bodies at zero angle of attack

G. E. Kaattari

NASA Technical Reports Server (NASA) · 1968 · 15 citations · 3 references

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Abstract

Relationship of shock standoff distance, at sonic and stagnation points, to body geometry of blunt bodies at zero angle of attack

References

3

Supersonic Flow past a Family of Blunt Axisymmetric Bodies

Milton D. Vandyke, Helen D. Gordon · NASA STI Repository (National Aeronautics and Space Administration) · 1959 · 79 citations · Full text

, , +7

An Approximate Solution of the Direct Supersonic Blunt-Body Problem for Arbitrary Axisymmetric Shapes

S. C. Traugott · Journal of the aerospace sciences/Journal of the aero/space sciences · 1960 · 46 citations

, , +15

Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at Mach 10.5

M. Inouye, J. G. Marvin, A.R. Sinclair · NASA Technical Reports Server (NASA) · 1968 · 10 citations · Full text

, , +9