Challenges in modeling the X-29A flight test performance-Reference-Cited by-同舟云学术

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Challenges in modeling the X-29A flight test performance

Published:1987-03-24 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

HICKS JOHN¹,KANIA JAN²,PEARCE ROBERT³,MILLS GLEN³

Affiliation:

1. NASA, Flight Research Center, Edwards, CA

2. USAF, Flight Test Center, Edwards AFB, CA

3. Grumman Aerospace Corp., Edwards, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1987-81

Reference12 articles.

1. tional Force and Moment Slipplemental Transonic Wind Tunnel Test Results, NASA TM-85909, 1984.

2. ZArnaiz, H.H. "Fliqht-Measured L i f t and Draq Characteristics of a Larye, Flexible, High Supersonic Cruise Airplane,'' NASA TM-X-3532, 1977.

3. 4Peterson. J.B. Jr., Mann, M.J. Sorrells, R.K., I l l , Sawyer, W.C., and Fuller, D.E. "Wind-TunnelIFlight Correlation Study of Aerodynamic Characteristics of a Large Flexible Supersonic Cruise Airplane (XB-70-1): Part 11 -Extrapolation o f Wind-Tunnel Data to Full-Scale Conditions." NASA TP-1515, 1980.

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. Development of a real-time aeroperformance analysis technique for the X-29A advanced technical demonstrator;Journal of Aircraft;1990-07

2. Flight test techniques for the X-29A aircraft;25th AIAA Aerospace Sciences Meeting;1987-03-24

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