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Numerical studies of the hypersonic strong interaction boundary-layer equations

M. J. Werle, +1 more
- 01 Oct 1971 - 
- Vol. 9, Iss: 10, pp 2058-2060
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This article is published in AIAA Journal.The article was published on 1971-10-01. It has received 9 citations till now. The article focuses on the topics: Blasius boundary layer & Boundary layer.

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Citations
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Journal ArticleDOI

Numerical solution of the hypersonic viscous shock-layer equations

R. T. Davis
- 01 May 1970 - 
TL;DR: Viscous shock layer equations of laminar hypersonic flow past blunt body at moderate to high Reynolds numbers were given in this article, where the body was assumed to have a blunt body.
Journal ArticleDOI

Initial conditions for the hypersonic-shock/boundary-layer interaction problem.

M. J. Werle, +2 more
- 01 Apr 1973 - 
TL;DR: In this article, boundary layers interacting with a hypersonic mainstream over hot and cold flat plates are solved numerically using an implicit finite-difference scheme, and the exact starting model is investigated and applied over a representative range of wall temperatures.
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Numerical Study of Strong Slot Injection into a Supersonic Laminar Boundary Layer

Michele Napolitano
- 01 Jan 1980 - 
TL;DR: In this article, the authors considered the problem of strong slot injection into a supersonic laminar boundary layer within the framework of triple-deck theory, and provided analytical solutions for the linearized equations, valid when the injection velocity is small in the triple deck scaling.
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Entropy layer effects in constant pressure hypersonic boundary layers.

P. A. Sullivan, +1 more
- 01 May 1973 - 
Journal ArticleDOI

Postbuckling Behavior of Orthotropic Skew Plates

K. A. V. Pandalai, +1 more
- 01 May 1973 - 
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

Numerical solution of the hypersonic viscous shock-layer equations

R. T. Davis
- 01 May 1970 - 
TL;DR: Viscous shock layer equations of laminar hypersonic flow past blunt body at moderate to high Reynolds numbers were given in this article, where the body was assumed to have a blunt body.
Journal ArticleDOI

Boundary-Layer Displacement and Leading-Edge Bluntness Effects in High-Temperature Hypersonic Flow

Hsien K. Cheng
- 01 May 1961 - 

Computation of the compressible laminar boundary-layer flow including displacement-thickness interaction using finite-difference methods

I. Fluegge-Lotz, +1 more
TL;DR: In this article, the boundary-layer equations are modified using the Howarth-Dorodnitsyn transformation, which results in equations advantageous for numerical computation when the flow is hypersonic.