Design of Nozzles for the Individual Cylinder Exhaust Jet Propulsion System
Description:
Report presenting an examination of the design of exhaust-stack nozzles for individual cylinder exhaust-gas jet propulsion and the results of tests on the effect of nozzle area on jet thrust and engine power. A satisfactory method of correlatig the test data for various engine-operating conditions is developed.
Date:
April 1941
Creator:
Pinkel, Benjamin; Turner, L. Richard & Voss, Fred
Item Type:
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Partner:
UNT Libraries Government Documents Department