Abstract
A method is proposed for calculating the two-dimensional nonviscous flows in ejector nozzles of arbitrary shape, for two operating cycles: the subsonic flow cycle of a secondary stream and a cycle when the secondary stream attains critical velocity, i.e., it is cut off. In the second case, the possibility is allowed for the appearance of a direct compression shock in the supersonic part of the secondary stream.
Keywords
Critical Velocity Arbitrary Shape Compression Shock Operating Cycle Direct Compression
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Literature cited
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Copyright information
© Plenum Publishing Corporation 1975