Results obtained in ballistics range facilities at U S Naval Ordnance Laboratory are presented relative to effects of Mach number, Reynolds number, and wall-to-stagnation enthalpy ratio on laminar-to-turbulent wake flow transition and on base flow geometry; effects of wall-to-stagnation enthalpy can be obtained by adjusting ambient temperature in ballistics range; results reported were obtained from measurements and observations made on shadowgraphs and schlieren photographs of flow.
Aerodynamic characteristics of hypersonic wakes
AIAA J
AIAA Journal ; 5 , n 9
1967
7 pages
Article (Journal)
English
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Aerodynamic characteristics of hypersonic wakes.
AIAA | 1967
|Engineering Index Backfile | 1964
|AIAA | 1964
|NTIS | 1963
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