Numerical Simulation of Combustion Phenomena
DOI: 10.1007/bfb0008659
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Unsteady combustion of solid propellants

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Cited by 13 publications
(2 citation statements)
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“…During oscillatory combustion, the acoustic wave present in the flow field increases the thermal conductivity of the propellant by 10-15 % which in turn increases the propellant surface temperature [32]. At low excited frequencies, there could be a possibility of the energy transfer from acoustics to propellant flame which may enhance the burning rates, as pointed out [8].…”
Section: Full Papermentioning
confidence: 93%
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“…During oscillatory combustion, the acoustic wave present in the flow field increases the thermal conductivity of the propellant by 10-15 % which in turn increases the propellant surface temperature [32]. At low excited frequencies, there could be a possibility of the energy transfer from acoustics to propellant flame which may enhance the burning rates, as pointed out [8].…”
Section: Full Papermentioning
confidence: 93%
“…The tangential mode of acoustic oscillation also affects the mean burning rates which were reported by Browniee and Marble [7] under high frequency combustion instability conditions, which shows large variation in mean burning rates. Chung and Kim [8] observed that the natural frequency of flame zone always lies between 1 and 100 Hz as peak frequency. This peak frequency of reaction zone encourages the energy transfer between acoustic wave and combustion flame zone likely to occur in low frequency regions leading to combustion instability as observed in experiment and actual flight conditions as well.…”
Section: Introductionmentioning
confidence: 99%