Find the approximate resonance frequencies

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Reference no: EM131401210

Explain how the three frequencies from Problem 1 will change with combustion temperature, chamber pressure, chamber length, chamber diameter, and throat diameter.

Problem 1

For a particular liquid propellant thrust chamber the following data are given:

Assume the gas composition and temperature to be uniform in the cylindrical chamber section. State any other assumptions that may be needed. Determine the approximate resonance frequencies in the first longitudinal mode, radial mode, and tangential mode.

Reference no: EM131401210

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