Viscous, Hypersonic Flow Around a Blunt Body
Viscous, Hypersonic Flow Around a Blunt Body

Author: John Edward Kaiser

Publisher:

Published: 1968

Total Pages: 182

ISBN-13:

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A simplified form of the Navier-Stokes equations was used to describe the flow in the shock layer of a blunt body. The equations are solved near the axis of the body by using the method of series truncation. The main method of solution is a finite difference method, which in principle allows one to handle axisymmetric bodies of arbitrary shape. The body shape is assumed to be given and the bow shock shape is determined step by step. (Author).

Two-dimensional Viscous Hypersonic Flow Over Simple Blunt Bodies Including Second-order Effects
Two-dimensional Viscous Hypersonic Flow Over Simple Blunt Bodies Including Second-order Effects

Author: Torstein Kjell Fannelöp

Publisher:

Published: 1964

Total Pages: 232

ISBN-13:

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Contents: First- and second-order boundary-layer theory fundamental equations and parameters; Finite-difference methods; Solutions to the first- and second-order equations near a plane stagnation point; Some first-order finite-difference solutions; Complete first- and second-order boundary-layer solutions for simple blunt bodies in hypersonic flow.