Integrated Flight Dynamic Modeling of Flexible Aircraft with Inertial Force-Propulsion-Aeroelastic Coupling-Reference-Cited by-同舟云学术

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Integrated Flight Dynamic Modeling of Flexible Aircraft with Inertial Force-Propulsion-Aeroelastic Coupling

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Nguyen Nhan¹

Affiliation:

1. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-194

Reference20 articles.

1. Application of Active Flexible Wing technology to the Agile Falcon

2. 2Wilson,J.R."ActiveAeroelastic Wing: aNew/Old TwistonFlight", AerospaceAmerica,September2002.

3. Aircraft aeroservoelastic compensation using constrained optimization

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