Subsonic calibration of the NASA Glenn Research Center 10- by 10-foot Supersonic Wind Tunnel (1998 test)-Reference-Cited by-同舟云学术

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Subsonic calibration of the NASA Glenn Research Center 10- by 10-foot Supersonic Wind Tunnel (1998 test)

Published:2000-06-19 Issue: Volume: Page:
ISSN:
Container-title:21st Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Arrington E.¹,Gonsalez Jose¹,Curry III Monroe¹

Affiliation:

1. Dynacs Engineering Co., Inc., Brook Park, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-2448

Reference37 articles.

1. Improved Speed Control System for an 87.000 HP Wind Tunnel Drive. NASA TM-106840, 1995.

2. NASA Lewis' 8x6 Transonic Wind Tunnel through Drive System Modifications. NASA CR-198455, 1996.

3. Quality Surveys of the NASA Lewis Research Center 10- by JO-Foot Supersonic Wind Tunnel. NASA CR-97-206326, 1998.

4. IO-by IO-Foot Supersonic Wind Tunnel. NASA TM-105626. 1995.

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. Recommended Practice: Calibration of Subsonic and Transonic Wind Tunnels (AIAA R-093-2003(2018));Recommended Practice: Calibration of Subsonic and Transonic Wind Tunnels (AIAA R-093-2003(2018));2003-01

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