The problem of hypersonic stagnation line merged-layer flow of variously shaped blunt asisymmetric bodies is here formulated in such a way as to allow analytical calculations for bodies generated by a conic section. The governing equations encompass, apart from the usual parameters, the eccentricity of the conic section that generates the body-of-revolution for the effect of body shape on the solution obtained. The stagnation-point surface pressure increases as the favorable pressure gradient decreases, in the course of a change of body shape from spherical to hyperboloid.
Hypersonic stagnation line merged layer flow on blunt axisymmetric bodies of arbitrary shape
AIAA, Thermophysics Conference ; 1993 ; Orlando, FL, United States
1993-07-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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