Add to ORKGA guide to a computer program, written in FORTRAN 4, for predicting the flow properties of turbulent mixing with combustion of a circular jet of hydrogen into a co-flowing stream of air is presented. The program, which is based upon the Imperial College group's PASSA series, solves differential equations for diffusion and dissipation of turbulent kinetic energy and also of the R.M.S. fluctuation of hydrogen concentration. The effective turbulent viscosity for use in the shear stress equation is computed. Chemical equilibrium is assumed throughout the flow
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Work performed during the first six months of the project duration for NASA Grant (NAG-1-861) is rep...
Computer program subroutines provide the thermodynamic and transport properties of hydrogen in tabul...
"Prepared by Fluid Mechanics and Thermal Systems, Inc. ... for Langley Research Center."Cover title....
The nonequilibrium flow field resulting from the turbulent mixing and combustion of a supersonic axi...
The kinetic theory of turbulent flow was employed to study the mixing limited combustion of hydrogen...
Analysis of compressible turbulent mixing of parallel coaxial hydrogen-air jets at supersonic spee...
A computer program based on a finite-difference, implicit numerical integration scheme is described ...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Simplified equilibrium hydrocarbon-air combustion gas model for use in air breathing engine cycle co...
The ALMA (axi-symmetrical lateral momentum analyzer) program is concerned with the computation of tw...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Work performed during the first six months of the project duration for NASA Grant (NAG-1-861) is rep...
Computer program subroutines provide the thermodynamic and transport properties of hydrogen in tabul...
"Prepared by Fluid Mechanics and Thermal Systems, Inc. ... for Langley Research Center."Cover title....
The nonequilibrium flow field resulting from the turbulent mixing and combustion of a supersonic axi...
The kinetic theory of turbulent flow was employed to study the mixing limited combustion of hydrogen...
Analysis of compressible turbulent mixing of parallel coaxial hydrogen-air jets at supersonic spee...
A computer program based on a finite-difference, implicit numerical integration scheme is described ...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Simplified equilibrium hydrocarbon-air combustion gas model for use in air breathing engine cycle co...
The ALMA (axi-symmetrical lateral momentum analyzer) program is concerned with the computation of tw...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Work performed during the first six months of the project duration for NASA Grant (NAG-1-861) is rep...
Computer program subroutines provide the thermodynamic and transport properties of hydrogen in tabul...