Effect of Passive Bleed System on an Integrated Diverterless Supersonic Inlet-Reference-Cited by-同舟云学术

Effect of Passive Bleed System on an Integrated Diverterless Supersonic Inlet

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Masud Jehanzeb¹,Akram Farooq²

Affiliation:

1. Air University

2. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-920

Reference21 articles.

1. 1Simon, P. C.; Brown, D. W.; and Huff, R. G. "Performance of external-compression bump inlet at Mach numbers of 1.5 and 2.0" NACA Report NACA-RM-E56L19 (1957).

2. Tradeoffs in Jet Inlet Design: A Historical Perspective

3. 3Li, B., and Liang, D."Numerical simulation and experiment of integral flow field of diverterless supersonic inlet/forebody" (2009) Hangkong Xuebao/ActaAeronautica etAstronauticaSinica, 30(9), pp.1597-1604.

4. A Computational Study on the Efficiency of Boundary Layer Bleeding for the Supersonic Bump Type Inlet

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