Ejector-Nozzle Flow and Thrust for Choked Flow

[+] Author and Article Information
H. E. Weber

Research Equipment Development, Space Sciences Laboratory, Missile and Vehicle Department, General Electric Company, Valley Forge, Pa.

J. Basic Eng 83(3), 471-477 (Sep 01, 1961) (7 pages) doi:10.1115/1.3659006 History: Received August 01, 1960; Online November 04, 2011


A theory for the prediction of flow for fully choked divergent shroud nozzles has been compared with experiment and corrected empirically. The prediction of thrust has been extended to include both the underexpanded and overexpanded flow regimes in this type of nozzle. Comparisons with the theory have been made and good correlation found in both overexpanded and underexpanded regimes of flow.

Copyright © 1961 by ASME
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