Modified Combustion Efficiency Curve for High-Velocity Model Combustors Integrated with the Inlet
V. Yu. Aleksandrov, N. V. Kukshinov
Baranov Central Institute of Aviation Motors, Moscow, 111116 Russia
Keywords: кривая выгорания, полнота сгорания, высокоскоростная камера сгорания, combustion efficiency curve, combustion efficiency, high-velocity combustor
Abstract
The method of obtaining combustion efficiency curves for fuel mixtures proposed by Annushkin is modified on the basis of data of high-altitude tests of high-velocity combustors integrated with the inlet. The combustion efficiency curve of a hydrocarbon-air mixture obtained in this study can be applied for design of high-velocity combustors.
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