Adiabatic Wall Solutions for the Hypersonic Compressible Laminar Boundary-Layer Equations-Reference-Cited by-同舟云学术

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Adiabatic Wall Solutions for the Hypersonic Compressible Laminar Boundary-Layer Equations

Published:1970 Issue:5 Volume:13 Page:1142
ISSN:0031-9171
Container-title:Physics of Fluids
language:en
Short-container-title:Phys. Fluids

Author:

Rogers David F.

Publisher

AIP Publishing

Subject

General Engineering

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Near-similarity approximation for compressible, laminar boundary layers on adiabatic walls;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;1997-05-01

2. Pressure Gradient Effects on Laminar Boundary Layers at Large Prandtl Numbers;AIAA Journal;1979-11

3. Phenomenological theory of thermodynamic coupling in multicomponent compressible laminar boundary layers;Physics of Fluids;1976

4. Approximate Temperature Distribution for a Diffuse, Highly Reflecting Material;AIAA Journal;1972-09

5. A Finite-Difference Method for Boundary Layers with Reverse Flow;AIAA Journal;1972-09

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