Parametric Model Size Study of Wall Interference in the Boeing Transonic Wind Tunnel Using TRANAIR
Author:
Affiliation:
1. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2310
Reference21 articles.
1. Distributions Figure6 ModelScaleStudy, Configuration Planforms
2. Transport Configurations in BTWT igure 21
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2. References;Understanding Aerodynamics;2012-11-15
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4. Determination of Transonic Wind Tunnel Geometry and Studies on Wall Interference by Numerical Simulation;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
5. Uncertainty Evaluation of Wall Interference in a Large Transonic Wind Tunnel;27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2010-06-28
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