Tsien, H. S. (1952) The transfer functions of rocket nozzles. Journal of the American Rocket Society, 22 (3). pp. 139-143. ISSN 0095-9073 http://resolver.caltech.edu/CaltechAUTHORS:20091209-134942869
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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.
|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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|Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||George Porter|
|Deposited On:||10 Dec 2009 23:14|
|Last Modified:||26 Dec 2012 11:38|
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