Method for evaluating flow field around blunt nosed body of revolution, from stagnation pressure measurements and bow shock shape; results obtained by applying method to hemisphere cylinder body at 7.3 Mach are given and compared with results given by approximate theory.
Flow field about hemisphere-cylinder body at Mach number of 7.3
Sweden. Flygtekniska Forsoksanstalten -- Meddelande (Aeronautical Research Inst Report)
1962
14 pages
Report
English
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Investigation of flow over spiked-nose hemisphere-cylinder at mach number of 6.8
Engineering Index Backfile | 1959
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