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Research Papers

Radial Equilibrium in Supersonic Compressors

[+] Author and Article Information
A. G. Hammitt, S. M. Bogdonoff

Department of Aeronautical Engineering, Princeton University, Princeton, N. J.

J. Basic Eng 81(4), 552-557 (Dec 01, 1959) (6 pages) doi:10.1115/1.4008556 History: Received September 03, 1958; Published December 01, 1959; Online February 20, 2019

Abstract

The radial equilibrium of flow through nearly radial shock waves in supersonic compressors is considered. The most restricted useful cases for which equilibrium is possible are a normal shock in a rotor, an oblique shock in a stator, or a normal shock with variable total head in a stator. The equilibrium requirement restricts the range of solutions but many useful ones are still possible.

Copyright © 1959 by ASME
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