A mathematical model of low amplitude pulse combustion systems using a Helmholtz resonator-type approach-Reference-Cited by-同舟云学术

A mathematical model of low amplitude pulse combustion systems using a Helmholtz resonator-type approach

Published:1985-02 Issue:3 Volume:98 Page:379-401
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Lee J.H.,Dhar B.,Soedel W.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference15 articles.

1. Analytical and experimental performance of an explosion cycle combustion chamber for a jet-propulsion engine;Zipkin;National Advisory Committee on Aeronautics Technical Note No. 1702,1948

2. Effect of low-loss air valve on performance of 22-inch diameter pulse-jet engine;Bressman;National Advisory Committee on Aeronautics Wartime Report No. E-279,1945

3. A review of pulse combustor technology;Putnam,1979

4. A logically simple method for solving the gas dynamics of a pulsating combustor;Winiarski,1971

5. An analysis of pulse combustion burner;Ahrens,1978

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