Extending the Flight Mach Number of the SR-71 Inlet-Reference-Cited by-同舟云学术

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Extending the Flight Mach Number of the SR-71 Inlet

Published:2005-05-16 Issue: Volume: Page:
ISSN:
Container-title:AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference
language:
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Author:

Colville Jesse¹,Starkey Ryan¹,Lewis Mark¹

Affiliation:

1. University of Maryland

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-3284

Reference22 articles.

1. 1Clough, J., Modeling and Optimization of Turbine Based Combined Cycle Engine Performance, Master's Thesis,Universityof Maryland,2004.

2. Intake Aerodynamics, Second Edition

3. AIAA Education Series;Seddon J.,1993

4. 4Mahoney,J.J.,InletsforSupersonicMissiles,AIAAEducationSeries,1990.

Cited by 3 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 validation of a two-dimensional variable geometry inlet;International Journal of Turbo & Jet-Engines;2021-08-09

2. Design and Unsteady Numerical Simulation of Variable Geometry Inlet Using Dynamic Meshes;Lecture Notes in Electrical Engineering;2019

3. Experimental Analyses of Inlet Characteristics of an Airbreathing Missile with Boundary-Layer Bleed;Journal of Propulsion and Power;2015-01

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