ON THE CALCULATION OF THE SIMPLEST RAMJET-TYPE COMBUSTOR
LIBRARY OF CONGRESS WASHINGTON DC AEROSPACE INFORMATION DIV
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A calculation method for the simplest ramjet-type combustor is presented. The method consists in closing the system of the basic gas-dynamic equations of fuel-mixture flow within a cylindrical tube with a point-ignition source, by introducing an auxiliary condition which defines the dependence of the width of the combustion zone on the distance to the ignition source. The results of the calculation were compared with some experimental data and were found to be in good agreement with them.
- Combustion and Ignition
- Jet and Gas Turbine Engines