Pressure Measurements Onboard a Small-Scale Rotating Wind Tunnel Model for Jet/Fin Interaction-Reference-Cited by-同舟云学术

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Pressure Measurements Onboard a Small-Scale Rotating Wind Tunnel Model for Jet/Fin Interaction

Published:2002-06-24 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Beresh Steven¹,Amatucci Vincent¹,Henfling John¹,Erven Rocky¹,Bourdon Christopher¹

Affiliation:

1. Sandia National Laboratories

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-3137

Reference19 articles.

1. 2Lee, E. E. Jr, and Willis, C. M. "Interaction Effects of a Control Jet Exhausting Radially from the Nose of an Ogive-Cylinder Body at Transonic Speeds," NASATN D-3752, January1967.

2. Interaction of multiple supersonic jets with a transonic flowfield

Cited by 2 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. Penetration of a Transverse Supersonic Jet into a Subsonic Compressible Crossflow;AIAA Journal;2005-02

2. Penetration of a Transverse Supersonic Jet into a Subsonic Compressible Crossflow;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

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