Improved Methodology for Predicting the Force on Stalled Spinning Wings-Reference-Cited by-同舟云学术

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Improved Methodology for Predicting the Force on Stalled Spinning Wings

Published:2015-01-03 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Ragheb Adam¹,Selig Michael S.¹

Affiliation:

1. University of Illinois, Urbana-Champaign

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0548

Reference44 articles.

1. Stall/Spin Mitigation Flight Testing with a Subscale Aerobatic Aircraft

2. 2Zimmerman, C. H. “Preliminary Tests in the NACA Free-Spinning Wind Tunnel,” NACA Report 557, 1937.

3. 3Soule, H. A. and Scudder, N. F. “A Method of Flight Measurement of Spins,” NACA Report 377, 1931.

Cited by 1 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. Wind Tunnel Testing of Wings in Spin;54th AIAA Aerospace Sciences Meeting;2016-01-02

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