Laminar Boundary Layers Developed within Unsteady Expansion and Compression Waves-Reference-Cited by-同舟云学术

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Laminar Boundary Layers Developed within Unsteady Expansion and Compression Waves

Published:1972-04 Issue:4 Volume:10 Page:499-505
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

HALL J. GORDON¹

Affiliation:

1. State University of New York at Buffalo, Buffalo, N. Y.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference11 articles.

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. Design and fabrication of a 9.5-inch Mach-6 quiet-flow Ludwieg tube;20th AIAA Advanced Measurement and Ground Testing Technology Conference;1998-06-15

2. Numerical method for unsteady compressible boundary layers driven by compression or expansion wave;International Journal for Numerical Methods in Fluids;1991-09-20

3. Unsteady compressible laminar boundary-layer formed within a centered expansion wave;AIAA Journal;1987-11

4. Boundary-layer effect on pressure variations in expansion waves;Nuclear Engineering and Design;1984-01

5. Unsteady Compressible Laminar Boundary-Layer Flow within a Moving Expansion Wave;AIAA Journal;1981-12

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