Turbulent Mixing and Combustion of Multi-Phase Reacting Flows in Ramjet and Ducted Rocket Environment.
Final progress rept. 1 Apr 81-30 Sep 82,
NAVAL WEAPONS CENTER CHINA LAKE CA
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Experiments with gaseous fuels to establish the base for the multiphase fuel tests were completed for the axisymmetric-coaxial flow fields. Radial and axial profiles of pressure, velocity, species concentration and temperature were determined. Agreement between measured values velocity and temperature and computer predictions was, in general, reasonably good. Experiments to determine axial and radial temperature profiles with boron particle-laden fuels were started. Author
- Combustion and Ignition
- Jet and Gas Turbine Engines
- Solid Rocket Propellants