Theoretical Analysis of the Flow Field Over a Family of Ogive Bodies. Supplement.
ARMY MISSILE RESEARCH AND DEVELOPMENT COMMAND REDSTONE ARSENAL AL TECHNOLOGY LAB
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Local body surface pressure coefficients and Mach numbers are presented for tangent ogive bodies at Mach numbers from 2 to 4.5 and at 0 and 2 deg angle-of-attack. These data were obtained using the US Army Missile Research and Development Command three-dimensional method of characteristics computer code. This volume is intended to supplement MIRADCOM Technical Report TD-CR-77-5, published August 1977. Author
- Fluid Mechanics