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Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners, including a program description and listing

J. C. South
TLDR
The FORTRAN program for approximate calculation of supersonic ideal gas flow past blunt bodies with sonic corners shows good agreement with prior work on this topic.
Abstract: 
FORTRAN program for approximate calculation of supersonic ideal gas flow past blunt bodies with sonic corners

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Citations
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Journal ArticleDOI

Planetary-Entry Gas Dynamics

Peter A. Gnoffo
- 01 Jan 1999 - 
TL;DR: A review of planetary-entry gas dynamics is presented in this paper, where the evolution of a blunt-body flowfield from a free molecular flow environment to a continuum environment is described.
Journal ArticleDOI

Influence of sonic-line location on Mars Pathfinder Probe aerothermodynamics

Peter A. Gnoffo, +3 more
- 01 Mar 1996 - 
TL;DR: In this article, the authors obtained flowfield solutions over the Mars Pathfinder Probe spanning the trajectory through the Martian atmosphere at angles of attack from 0 to 11 degrees and derived two regions where the derivative of pitching moment with respect to angle of attack is positive at small angles of attacks.
Journal ArticleDOI

Surface recession rate of an ablating polymer.

Nelson H. Kemp
- 01 Sep 1968 - 
Journal ArticleDOI

The Impingement of a Uniform, Axisymmetric, Supersonic Jet on a Perpendicular Flat Plate

J. H. Gummer, +1 more
- 01 Nov 1971 - 
ReportDOI

Hypersonic Lifting Body Windward Surface Flow-Field Analysis for High Angles of Incidence

Jr. Adams, +2 more
TL;DR: In this paper, a windward surface flow-field analysis for general lifting body configurations at high angles of incidence under hypersonic perfect gas conditions is presented, where the boundary-layer analysis is based on the governing equations for yawed blunt body boundary layers.
References
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Hypersonic Flow Theory

Wallace D. Hayes, +1 more
Book

Hypersonic Flow Theory

Wallace D. Hayes, +3 more
TL;DR: Hypersonic flow theory, Hypersonic Flow Theory (HFT) as discussed by the authors, Hypeneric Flow theory (HYFT), Hypenergetic flow theory (HOFT)
Journal ArticleDOI

The supersonic blunt-body problem - Review and extension

Milton D. Van Dyke
- 01 Aug 1958 - 
Journal ArticleDOI

An Experimental Investigation of Blunt Body Stagnation Point Velocity Gradient

J. Christopher Boison
- 01 Feb 1959 - 
Journal ArticleDOI

An Approximate Solution of the Direct Supersonic Blunt-Body Problem for Arbitrary Axisymmetric Shapes

Stephen C. Traugott
- 01 May 1960 - 
TL;DR: The integral method of Belotserkovskii has been carried out to the first approximation for arbitrary blunt axisymmetric bodies in supersonic or hypersonic flight.