Methodology for the Design of Streamline-Traced External-Compression Supersonic Inlets-Reference-Cited by-同舟云学术

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Methodology for the Design of Streamline-Traced External-Compression Supersonic Inlets

Published:2014-07-25 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
language:
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Author:

Slater John W.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3593

Reference19 articles.

1. AIAA Education Series;Seddon J.,1985

2. AIAA Education Series;Seddon J.,1993

3. Development Program for the F-15 Inlet

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4. Design studies on NAGIC flowfield with application to integrated irregular-shaped supersonic inlet;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-08-29

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