Elastically Shaped Wing Optimization and Aircraft Concept for Improved Cruise Efficiency-Reference-Cited by-同舟云学术

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Elastically Shaped Wing Optimization and Aircraft Concept for Improved Cruise Efficiency

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Nguyen Nhan¹,Trinh Khanh²,Reynolds Kevin¹,Kless James³,Aftosmis Michael¹,Urnes James⁴

Affiliation:

1. NASA Ames Research Center

2. Stinger Ghaffarian Technologies, Inc.

3. Science and Technology Corporation

4. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-141

Reference17 articles.

1. Nguyen,N.,Nelson,A.,andPulliam,T.“DamageAdaptiveControlSystemResearchReport,”Internal NASAReport,April2006.

2. Miranda, L., Elliot, R., and Baker, W. “A Generalized Vortex Lattice Method for Subsonic and SupersonicFlowApplications,”NASA CR-2865, 1977.

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