Accession Number : ADA133802

Title :   Turbulent Mixing and Combustion of Multi-Phase Reacting Flows in Ramjet and Ducted Rocket Environment.

Descriptive Note : Final progress rept. 1 Apr 81-30 Sep 82,

Corporate Author : NAVAL WEAPONS CENTER CHINA LAKE CA

Personal Author(s) : Lee,M J ; Schadow,K C

PDF Url : ADA133802

Report Date : Oct 1982

Pagination or Media Count : 6

Abstract : 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)

Descriptors :   *Ramjet engines, *Ducted rockets, Combustors, Multiphase flow, Combustion, Gas generating systems, Jet mixing flow, Turbulent flow, Reaction kinetics, Solid rocket propellants, Flow visualization, Laser velocimeters, Doppler effect

Subject Categories : Combustion and Ignition
      Jet and Gas Turbine Engines
      Solid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE