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The transfer functions of rocket nozzles

Tsien, H. S. (1952) The transfer functions of rocket nozzles. Journal of the American Rocket Society, 22 (3). pp. 139-143. ISSN 0095-9073.

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The transfer function is defined as the fractional oscillating mass flow rate divided by the fractional sinusoidal pressure oscillation in the rocket combustion chamber. This is calculated as a function of the frequency of oscillation. For very small frequencies, the transfer function is approximately 1 with a small "lead component." For very large frequencies, the transfer function is considerably larger than 1, and is approximately 1 + (γM_1)^(-1) where γ is the ratio of specific heats of the gas, and M_l is the Mach nUlllber at entrance to the nozzle.

Item Type:Article
Additional Information:(Reprinted from Journal of the American Rocket Society, May-June, 1952). Copyright, 1952, by the American Rocket Society, Inc., and reprinted by permission of copyright owner. Received January 2, 1952.
Group:Guggenheim Jet Propulsion Center
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Other Numbering System NameOther Numbering System ID
Guggenheim Jet Propulsion Center19
Issue or Number:3
Record Number:CaltechAUTHORS:20091209-134942869
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Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:16928
Deposited By: George Porter
Deposited On:10 Dec 2009 23:14
Last Modified:03 Oct 2019 01:19

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