A Computational Study on the Efficiency of Boundary Layer Bleeding for the Supersonic Bump Type Inlet-Reference-Cited by-同舟云学术

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

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Lim Seol¹,Koh Dong Hoon¹,Kim Sang Dug²,Song Dong Joo¹

Affiliation:

1. Yeungnam University

2. Daegu University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-34

Reference14 articles.

1. 2Seddon,J.,andGoldsmith,E.L.,1999,IntakeAerodynamics,pp.336-340.

2. 3Nicolai,L.M.,1975,FundamentalofAircraftDesign,METSInc.SanJose,CA.

3. Airframe/propulsion integration of supersonic cruise vehicles

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3. Design and analysis of a hypersonic inlet with an integrated bump/forebody;Chinese Journal of Aeronautics;2019-10

4. Aerodynamic and Stealth Integrated Design of DSI Inlet by Surrogate-Based Multi-Objective Optimization with EHVI Infill Criterion;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2019-10

5. Pseudo-shock waves and their interactions in high-speed intakes;Progress in Aerospace Sciences;2016-04

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