Doublet-panel method for half-model wind-tunnel corrections
Author:
Affiliation:
1. National Research Council of Canada, Ottawa, Ontario, Canada
2. de Havilland Aircraft Company of Canada, Downsview, Ontario, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45448
Reference9 articles.
1. Wind-tunnel wall interference corrections for three-dimensional flows
2. 4Stakgold, I., Green's Functions and Boundary Value Problems, Wiley, New York, 1979, pp.513-514.
3. Experimental observations of wall interference at transonic speeds
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