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[American Institute of Aeronautics and Astronautics 11th Propulsion Conference - Anaheim,CA,U.S.A. (29 September 1975 - 01 October 1975)] 11th Propulsion Conference - Effect of Reynolds number on the nozzle afterbody performance of theAGARD nozzle afterbody and the B-1 0.06-scale model at transonic Mach numbers

✍ Scribed by ROBINSON, C.; PRICE, E.

Book ID: 121024943
Publisher: American Institute of Aeronautics and Astronautics
Year: 1975
Weight: 592 KB
Category: Article
DOI: 10.2514/6.1975-1321

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