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Perturbation analysis of one-dimensional heterogeneous flow in rocket nozzles

Rannie, W. D. (1962) Perturbation analysis of one-dimensional heterogeneous flow in rocket nozzles. In: Detonation and two-phase flow : a selection of technical papers based mainly on a symposium of the American Rocket Society held at Palm Beach, Florida, April 26-28, 1961. Academic Press , New York, pp. 117-144. ISBN 978-1-60086-261-8.

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A perturbation analysis of the velocity and temperature lags in two-phase flow in rocket nozzles is developed and applied to the calculation of specific impulse and other performance characteristics of nozzles of arbitrary shape. Within the limitations of the one-dimensional flow approximation, the analysis is valid for distributions of particle diameters that are in a practical range.

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Additional Information:© 1962, Submitted for publication to the American Rocket Society, Jan. 3, 1962. w. D. RANNIE is Robert H. Goddard Professor of Jet Propulsion, Daniel and Florence Guggenheim Jet Propulsion Center, Kármán Laboratory of Fluid Mechanics and Jet Propulsion.
Group:Guggenheim Jet Propulsion Center
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Guggenheim Jet Propulsion Center 130
Record Number:CaltechAUTHORS:20110121-101804833
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Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:21849
Deposited By: Ruth Sustaita
Deposited On:04 Feb 2011 20:23
Last Modified:03 Oct 2019 02:30

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