The Sychev (1960) analysis for inviscid hypersonic flow past slender bodies at large angle of attack is shown to be applicable to all slender-body flows whose crossflow Mach numbers are greater than sonic; it is therefore not restricted to flows with hypersonic crossflow Mach number values, as indicated elsewhere in the literature. It is also noted that the Sychev similarity applies to a number of slender-body flows with subsonic crossflow Mach numbers, including incompressible flow.
Extension of hypersonic, high-incidence, slender-body similarity
AIAA Journal ; 25
1987-11-01
Miscellaneous
No indication
English
Similarity solutions for hypersonic flow past slender bodies of revolution at small incidence
Online Contents | 1995
|Viscous hypersonic flow past a slender cone at incidence
AIAA | 1968
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