Aeroservoelastic Testing of a Sidewall Mounted Free Flying Wind-Tunnel Model-Reference-Cited by-同舟云学术

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

Published:2008-06-14 Issue: Volume: Page:
ISSN:
Container-title:26th AIAA Applied Aerodynamics Conference
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Author:

Scott Robert¹,Vetter Travis²,Penning Kevin³,Coulson David⁴,Heeg Jennifer¹

Affiliation:

1. NASA Langley Research Center

2. Northrop Grumman Corp.

3. Lockheed Martin

4. Analytical Services and Materials, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7186

Reference18 articles.

1. An Overview of SensorCraft Capabilities and Key Enabling Technologies

2. Aeroservoelastic Design and Test Validation of the Joined Wing Sensorcraft

3. Aerodynamic Cruise Design of a Joined Wing SensorCraft

4. 4Lockyer, 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.

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