Design, fabrication, and testing of the DARPA/Wright Lab 'smart wing' wind tunnel model-Reference-Cited by-同舟云学术

Design, fabrication, and testing of the DARPA/Wright Lab 'smart wing' wind tunnel model

Published:1997-04-07 Issue: Volume: Page:
ISSN:
Container-title:38th Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Kudva Jayanth¹,Appa Kari¹,Martin Christopher¹,Jardine A.¹,Kudva Jayanth¹,Appa Kari¹,Martin Christopher¹,Jardine A.¹,Sendeckyj George²,Harris Terry²,McGowan Anna-Marie³,Lake Renee³,Sendeckyj George²,Harris Terry²,McGowan Anna-Marie³,Lake Renee³

Affiliation:

1. Northrop Grumman Corp., Military Aircraft Systems Div., El Segundo, CA

2. USAF, Wright Lab., Wright-Patterson AFB, OH

3. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1198

Reference16 articles.

1. A flight research program for active aeroelastic wing technology

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