Session: The NASA CRM Model & High Reynolds Number Aerodynamics and Testing (Invited)
Published Online:3 Jan 2015https://doi.org/10.2514/6.2015-0619
- Cited by
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- 28 February 2017 | Journal of Aircraft, Vol. 54, No. 4
- Development of wing deflection assessment methods through experimental ground tests and finite element analysisThin-Walled Structures, Vol. 108
Copyright © 2015 by Stefan Keye. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.