Tables of Inviscid Supersonic Flow about Circular Cones at Incidence Gamma Equals 1.4. Part III.
ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)
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The report provides tabulated results for half cone angles of 45, 47.5, 50, 52.5, 55 and 57 degrees with Mach numbers ranging from 3 to 20.
- Fluid Mechanics