Parameters affecting penetration of a single jet into a supersonic crossflow - A CFD study. II-Reference-Cited by-同舟云学术

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Parameters affecting penetration of a single jet into a supersonic crossflow - A CFD study. II

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Roger R.¹,Chan S.²

Affiliation:

1. Johns Hopkins Univ., APL, Laurel, MD

2. SY Technology, Huntsville, AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-425

Reference67 articles.

1. Zukoski &Spaid (1964)

2. Strike (1968)

3. Povinellietal (1970)

4. Cohenetal (1971)

5. BiHigetal (1971)

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1. Numerical Study of Maneuverability Control in High-Speed Aero-vehicles Using Transverse Sonic Jet Injectors;AIAA SCITECH 2024 Forum;2024-01-04

2. Detailed flow physics of the supersonic jet interaction flow field;Physics of Fluids;2009-04

3. Numerical investigation of the shock interaction effect on the lateral jet controlled missile;Aerospace Science and Technology;2006-07

4. Measurement of Experimental Boundary Conditions for CFD Validation of a Supersonic Jet in Transonic Crossflow;25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2006-06-05

5. Penetration of a Transverse Supersonic Jet into a Subsonic Compressible Crossflow;AIAA Journal;2005-02

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