Both zero-order and first-order solution presented for 2-dimensional and axisymmetric hypersonic flow where M is free stream Mach number and delta is characteristic slope; solutions are compared with exact numerical integrations of equations of motion, and appear to be accurate particularly when shock is relatively close to body.
Approximate analytical solutions for hypersonic flow over slender power law bodies
NASA -- Tech Report
1959
24 pages
Report
English
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