Control of forward swept wing configurations dominated by flight-dynamic/aeroelastic interactions-Reference-Cited by-同舟云学术

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Control of forward swept wing configurations dominated by flight-dynamic/aeroelastic interactions

Published:1984-06-25 Issue: Volume: Page:
ISSN:
Container-title:17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference
language:
Short-container-title:

Author:

RIMER M.¹,CHIPMAN R.¹,MUNIZ B.¹

Affiliation:

1. Grumman Aerospace Corp., Bethpage, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1866

Reference12 articles.

1. Active control of aeroelastic divergence

2. Rigid body-structural mode coupling on a forward swept wing aircraft

3. Wilkinson, K. and Rauch, F. "Predicted and Measured Divergence Speeds of an Advanced Composite Forward Swept Wing Model," AFWALTR-80-3059.

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