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- W2080555144 abstract "Current theories concerning combustion instability in rocket motors involve the concept of a time delay between the instant of injection of a propellant element into the combustion chamber and its final evolution into hot gases. In order to apply these theories to actual design problems, it is first necessary to determine experimentally the time lag and several associated parameters for each class of propellants and chamber configurations. These measurements are now being made on a bipropellant chamber at Princeton as the second phase of a program whose ultimate objective is to provide the information necessary to direct the design 01 development of rocket engines toward suppression of high-frequency combustion instability. The introductoiy phase of this program, described in Ref. (2), dealt with the development of an experimental technique and instrumentation capable of providing the necessary data. The current paper presents some preliminary results of the second phase, in which these techniques have been used to determine the combustion chamber transfer function of a particular bipropellant configuration and the deduction therefrom of the time lag and related parameters. A brief recapitulation of the conceptual background is given, together with the methods used to obtain the desired measurements. Some of the limitations of these deduced results are discussed, and current methods for reducing the limitations are described." @default.
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- W2080555144 date "1956-01-01" @default.
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- W2080555144 title "Measurements of the Combustion Time Lag in a Liquid Bipropellant Rocket Motor" @default.
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- W2080555144 doi "https://doi.org/10.2514/8.6907" @default.
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