2021
DOI: 10.1590/jatm.v13.1198
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Investigations on Complex Acoustic Modes of Rocket Engines Combustion Chambers for Damping Allocation

Abstract: Combustion instability can severely impair the operation of many kinds of combustion engines. Acoustic resonators are widely used to suppress the pressure oscillations caused by the coupling between the combustion process and the combustion chamber acoustic modes. Combustion chambers with subsonic flow in its inlets and outlets, like gas turbine combustors, exhibit some acoustical damping due to the presence of openings. In such chambers, the acoustic modes are complex. In a complex mode, the antinode regions … Show more

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(2 citation statements)
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“…According to Planck's law of radiation, the spectral radiance of absolute temperature T can be expressed by formula (1):…”
Section: Establishment Of Multi-channel Temperature Measurement Modelmentioning
confidence: 99%
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“…According to Planck's law of radiation, the spectral radiance of absolute temperature T can be expressed by formula (1):…”
Section: Establishment Of Multi-channel Temperature Measurement Modelmentioning
confidence: 99%
“…High-speed dynamic temperature measurement has a wide range of needs in engineering, such as rocket engine combustion, aero engine combustion, ammunition detonation, laser processing, etc. [1][2][3]. In the field of temperature measurement, compared with other temperature measurement methods, multispectral temperature measurement is based on Planck's law of radiation, and the temperature value can be inferred through the intensity of radiation and multiple sets of wavelengths.…”
Section: Introductionmentioning
confidence: 99%