Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Reference11 articles.
1. The correction of wind tunnel nozzles for two-dimensional, supersonic flow
2. LaBerge, J. G., Design, Calibration and Correction of a 1.6 Mach Number Nozzle, National Aeronautical Establishment of Canada, Laboratory Report LR-41, November5,1952. (ASTIA No.AD-2068.)
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2 articles.
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