Survey of the accoustic near field of three nozzles at a pressure ratio of 30
1957
32 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Accoustic Analysis of Combustion Engines
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Effect of Mach number on the accoustic field of 2:1 elliptic-slot jet
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|Advanced high area ratio nozzles
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|