The enhancement of the mixing and combustion processes in supersonic flow applied to scramjet engine

Conference · Wed Jul 01 00:00:00 EDT 1992

OSTI ID:6959243

Kopchenov, V I; Lomkov, K E ^[1]

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1. Tsentral'nyi NII Aviatsionnogo Motorostroeniia, Moscow (Russian Federation)

The Reynolds averaged parabolized Navier-Stokes equations are employed for the numerical study of turbulent mixing and combustion of a supersonic hydrogen jet in a supersonic airflow. A one-equation differential turbulence model is utilized. The simplified flame sheet model is employed for the numerical simulation of the supersonic combustion. 24 refs.

• OSTI ID: 6959243
• Report Number(s): AIAA-Paper-92-3428; CONF-920747-
• Resource Relation: Conference: 28. joint propulsion conference, Nashville, TN (United States), 6-8 Jul 1992
• Country of Publication: United States
• Language: English

Related Subjects

33 ADVANCED PROPULSION SYSTEMS
RAMJET ENGINES
COMBUSTION KINETICS
SUPERSONIC FLOW
AIR FLOW
COMPUTERIZED SIMULATION
HYDROGEN
MATHEMATICAL MODELS
MIXING
NAVIER-STOKES EQUATIONS
NOZZLES
TURBULENCE
CHEMICAL REACTION KINETICS
DIFFERENTIAL EQUATIONS
ELEMENTS
ENGINES
EQUATIONS
FLUID FLOW
GAS FLOW
HEAT ENGINES
INTERNAL COMBUSTION ENGINES
KINETICS
NONMETALS
PARTIAL DIFFERENTIAL EQUATIONS
REACTION KINETICS
SIMULATION
330100* - Internal Combustion Engines