Wind Tunnel Support System Influence on NASA Common Research Model at Low-Speed Conditions
Author:
Affiliation:
1. University of Stuttgart, 70569 Stuttgart, Germany
Funder
FP7 Research infrastructures
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034440
Reference27 articles.
1. A numeric far field model for support interference studies in a slotted wall wind tunnel (European Transonic Windtunnel)
2. KuehnW. “FLIRET Final Publishable Report,” Airbus Deutschland TR AST4-CT-2005-516118, Hamburg, Germany, 2010.
3. The FALCON 7X: From ETW to Flight
4. Wall and Support Interference Corrections of NASA Common Research Model Wind Tunnel Tests in JAXA
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