Model Deformation Measurements of the Truss-Braced Wing Aircraft in the NASA Ames 11-By 11-Ft Transonic Wind Tunnel-Reference-Cited by-同舟云学术

Model Deformation Measurements of the Truss-Braced Wing Aircraft in the NASA Ames 11-By 11-Ft Transonic Wind Tunnel

Published:2017-01-05 Issue: Volume: Page:
ISSN:
Container-title:55th AIAA Aerospace Sciences Meeting
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Author:

Drain Bethany A.¹,Kushner Laura K.¹,Schairer Edward T.²,Heineck James T.²

Affiliation:

1. Aerospace Computing, Inc.

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2017-1054

Reference14 articles.

1. Bradley, M. K. and Droney, C. K. "Subsonic Ultra Green Aircraft Research: Phase I Final Report," NASA Contractor Report NASA/CR-2011-216847, Boeing Research and Technology, April 2011.

2. 2Bradley, M. K., Droney, C. K., and Allen, T. J. "Subsonic Ultra Green Aircraft Research Phase II: N+4 Advanced Concept Development," NASA Contractor Report NASA/CR-2012-217556, Boeing Research and Technology, May

3. Videogrammetric Model Deformation Measurement Technique for Wind Tunnel Applications

4. Model Deformation Measurement (MDM) at Onera

5. Model Deformation Measurement Capabilities at ETW

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