2010-4344 The Effect of Diffuser Geometry on the Starting Pressure Ratio of a Supersonic Wind Tunnel
27th, Aerodynamics measurement and ground testing conference ; 2010 ; Chicago, IL
01.01.2010
10 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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DataCite | 1928
Combustion-driven M3 Supersonic Wind Tunnel with Diffuser-Ejector
British Library Conference Proceedings | 1994
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AIAA | 1971
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