Affiliation:
1. The Rand Corporation, Santa Monica, CA
Abstract
An attractive feature of the plug-type nozzle for turbojets and rocket jets is that it can automatically adjust its effective exit area with operating pressure ratio and achieve a high level of efficiency over a wide range of operating pressure ratio without variation of mechanical shape. The design and off-design performance analysis of such nozzles is described.
Publisher
American Society of Mechanical Engineers
Cited by
4 articles.
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