Numerical Investigation of Wall Mounting Effects in Semi-Span Wind-Tunnel Tests
Author:
Affiliation:
1. École de Technologie Supérieure
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2025
Reference26 articles.
1. The aerodynamic design of multi-element high-lift systems for transport airplanes
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1. Improvement of Wall-Corrections at the National Research Council’s Trisonic Wind Tunnel;Journal of Aircraft;2019-11
2. Study of the Subsonic Wall Interference in Stall of the NASA CRM at the NRC 1.5 m Trisonic Wind Tunnel;33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2017-06-02
3. Preliminary investigation on stall characteristics of a Regional BWB for low speed approach;35th AIAA Applied Aerodynamics Conference;2017-06-02
4. Towards the Use of CFD to Improve and Validate the Wall Correction Methodology at the NRC 1.5 m Trisonic Wind Tunnel;32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2016-06-10
5. Comparison of data correction methods for blockage effects in semispan wing model testing;EPJ Web of Conferences;2016
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