High frequency combustion instability in liquid propellant rocket engines - A review of studies carried out at ONERA for the Ariane launcher

Habiballah, Mohammed; Dubois, I.; Vingert, Lucien; Lourme, D.; Scherrer, Dominique

doi:10.2514/6.1992-774

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1993

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“…3 Until now, stability assessment of rocket engines has relied on qualitative tools and full-scale testing. Much of this work was compiled by Harrje and Reardon.…”

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confidence: 99%

Combustion Instability Analysis: Numerical Analysis of Engine Instability

1995

Liquid Rocket Engine Combustion Instability

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Nomenclature b = chamber width D = species diffusivity D m = diameter of group m droplets e = gas-phase specific internal energy h k = specific enthalpy of species k MK = molar mass of species k n m = number of group m droplets per unit volume p = pressure R = perfect gas constant T = temperature t = time u = axial gas velocity u m = axial droplet velocity V = gas velocity V m = droplet velocity v = transverse gas velocity v m = transverse droplet velocity x = axial direction y = transverse direction z = radial direction A = thermal conductivity H = viscosity p = gas-phase density p k = partial density of species k p L = liquid density

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“…3 Until now, stability assessment of rocket engines has relied on qualitative tools and full-scale testing. Much of this work was compiled by Harrje and Reardon.…”

mentioning

confidence: 99%