Design, development, and testing of an active flutter margin augmentation system for a commercial transport airplane-Reference-Cited by-同舟云学术

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Design, development, and testing of an active flutter margin augmentation system for a commercial transport airplane

Published:1979-04-04 Issue: Volume: Page:
ISSN:
Container-title:20th Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

OCONNELL R.¹,MESSINA A.¹

Affiliation:

1. Lockheed-California Co., Burbank, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1979-790

Reference5 articles.

1. The use of probability analysis in aircraft certification and its effects on maintenance and equipment maintenance

2. Dynamic gust, landing, and taxi loads determination in the design ofthe L-1011.

Cited by 4 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. Reducing Induced Drag and Maneuver Loads by Active Aeroelastic Alteration;Journal of Aircraft;2016-11

2. Design and flight test of active flutter suppression on the X-56A multi-utility technology test-bed aircraft;The Aeronautical Journal;2016-05-10

3. Erweiterung der Einsatzgrenzen;Flugregelung;2011

4. ATTAS flight test and simulation results of the advanced gust management system LARS;Guidance, Navigation and Control Conference;1992-08-10

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