NASA Technical Reports Server (NTRS) : Computations pdf

NASA Technical Reports Server (NTRS) : Computations

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Description of the Book:

The computer programs developed for computation of viscous shock layer flow distribution surrounding the nose of a shuttle orbiter during reentry are presented. The problem formulation and the numerical procedures used to solve the basic set of equations are described. The results of flow distribution properties at several trajectory points, ranging from the high altitude rarefied region to the low altitude boundary layer region are analyzed

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 2/1/1973
• Year: 1973
• Book Topics/Themes: NASA Technical Reports Server (NTRS), ATMOSPHERIC ENTRY, FLOW DISTRIBUTION, FLOW EQUATIONS, NOSE CONES, SPACE SHUTTLE ORBITERS, BOUNDARY LAYER FLOW, COMPUTER PROGRAMS, REENTRY PHYSICS, VISCOUS FLOW, Li, C. P

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