The effects of attack angle on aerodynamic interaction due to side jet from a blunted body in a supersonic flow-Reference-Cited by-同舟云学术

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The effects of attack angle on aerodynamic interaction due to side jet from a blunted body in a supersonic flow

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Kurita Mitsura¹,Okada Takumi¹,Nakamura Yoshiaki¹

Affiliation:

1. Nagoya Univ., Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-261

Reference21 articles.

1. 44-50.

2. Two-dimensional jet interaction studies at large values of Reynolds and Mach numbers

3. Experimental investigation of side-jet steering for supersonic and hypersonic missiles

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