Preliminary Design of a 2D Supersonic Inlet to Maximize Total Pressure Recovery-Reference-Cited by-同舟云学术

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Preliminary Design of a 2D Supersonic Inlet to Maximize Total Pressure Recovery

Published:2005-09-26 Issue: Volume: Page:
ISSN:
Container-title:AIAA 5th ATIO and16th Lighter-Than-Air Sys Tech. and Balloon Systems Conferences
language:
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Author:

Ran Hongjun,Mavris Dimitri

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-7357

Reference2 articles.

1. 6AMES Research Staff, "Equations, Tables, and Charts for Compressible Flow", NACA Report 1135,National Advisory Committee forAeronautics, 1953.

2. 8Crosthwait, E.L., Kennon, I.G., Jr. "Preliminary design Methodology for Air-Induction Systems", Technical Report SEG-TR-67-1, Systems Engineering Group, 1967.

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