Loads Model Development and Analysis for the F/A-18 Active Aeroelastic Wing Airplane-Reference-Cited by-同舟云学术

Loads Model Development and Analysis for the F/A-18 Active Aeroelastic Wing Airplane

Published:2005-06-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
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Author:

Allen Michael¹,Lizotte Andrew¹,Dibley Ryan¹,Clarke Robert¹

Affiliation:

1. NASA Dryden Flight Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6313

Reference11 articles.

1. The Active Aeroelastic Wing Flight Research Program - Technical program and model analytical development

2. Development and Testing of Control Laws for the Active Aeroelastic Wing Program

3. 4Lewis, G. E. "AFTI/F-111 Mission Adaptive Wing Maneuver Load Control," available from the NASA Center for AeroSpace Information (CASI), CASI document identification 19910074478.

4. Helicopter flight data feature extraction or component load monitoring

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5. Flight Test of the F/A-18 Active Aeroelastic Wing Airplane;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2005-06-19