Aeroservoelastic Wind-Tunnel Tests of a Free-Flying, Joined-Wing SensorCraft Model for Gust Load Alleviation-Reference-Cited by-同舟云学术

Aeroservoelastic Wind-Tunnel Tests of a Free-Flying, Joined-Wing SensorCraft Model for Gust Load Alleviation

Published:2011-04-04 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
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Author:

Scott Robert¹,Coulson David²,Castelluccio Mark³,Heeg Jennifer¹

Affiliation:

1. NASA Langley Research Center

2. Analytical Services & Materials, Inc.

3. Analytical Services & Materials, Inc

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1960

Reference30 articles.

1. An Overview of SensorCraft Capabilities and Key Enabling Technologies

2. 2Lockyer, A. J., Drake, A., Bartley-Cho, J., Vartio, E., Solomon, D., and Shimko, T. “HIGH LIFT OVER DRAG ACTIVE (HiLDA) WING; Delivery Order 0007:HiLDA Wing Program,” Tech. Rep. AFRL-VA-WP-TR-2005-3066, Northrop Grumman Corporation, 2005.

3. Aeroservoelastic Testing of a Sidewall Mounted Free Flying Wind-Tunnel Model

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