Problems of Thermodynamic Equilibrium of Outflowing Combustion Products,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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The goals of the present study were to measure translatory temperature, identify the radiation spectrum of a stream of combustion products from condensed systems behind the edge of the nozzle in a model engine, and establish the equilibrium condition of the system, provided it exists. The radiation spectrum of combustion products flowing from a model jet engine nozzle was studied for ballistiteH powder and a composition of H5 aluminum for two engine operating modes incomplete 20-30 at and complete 80-90 at.
- Atomic and Molecular Physics and Spectroscopy
- Combustion and Ignition