Application of wall interference corrections to a low aspect ratio airfoil model
Author:
Affiliation:
1. National Defense Academy, Yokosuka, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-716
Reference24 articles.
1. Preliminary Test Results of NDA Cryogenic Wind Tunnel and Its System
2. Characteristics of a cryogenic wind tunnel at National Defense Academy. (Part 2). Tunnel characteristics at ambient and cryogenic temperatures.
3. Preliminary airfoil testing experience in the NDA cryogenic wind tunnel
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