Add to ORKGShear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engine exhaust plume analysi
An investigation of oxygen compatibility and resistance to ignition of candidate materials for use i...
Modified P function applied to turbulent mixing of three coaxial, axisymmetric jets of reactive gase
Liquid propellant rocket engine performance computer program with distributed energy releas
As part of a continuing study of the environmental effects of solid rocket motor (SRM) operations in...
Experimental droplet burning rates obtained at atmospheric pressure in combustion gas environmen
Model for prediction of rocket engine combustion with performance parameters of gas phase turbulent ...
Hydrogen fuel combustion hazard and venting problems from launch vehicles in hypersonic air flo
A computationally-viable model describing the interaction between fluid-mechanical turbulence and fi...
A series of fundamental problems related to jet engine air pollution and combustion were examined. T...
A viewgraph presentation describing experimental results and analytical developments about plume dia...
Idealized combustion model in which exothermic or endothermic reactions are permitted at or very nea...
The mathematical and physical basis of the SHIP computer program which embodies a finite-difference,...
The space station uses small rocket motors, called thrusters, for orientation control. Because of th...
Interacting two-phase flow in four differently sized pneumatic two-fluid atomizers was investigated ...
Chemical and chemical radiative effects on base flow field of multiple nozzled launch vehicles of Sa...
An investigation of oxygen compatibility and resistance to ignition of candidate materials for use i...
Modified P function applied to turbulent mixing of three coaxial, axisymmetric jets of reactive gase
Liquid propellant rocket engine performance computer program with distributed energy releas
As part of a continuing study of the environmental effects of solid rocket motor (SRM) operations in...
Experimental droplet burning rates obtained at atmospheric pressure in combustion gas environmen
Model for prediction of rocket engine combustion with performance parameters of gas phase turbulent ...
Hydrogen fuel combustion hazard and venting problems from launch vehicles in hypersonic air flo
A computationally-viable model describing the interaction between fluid-mechanical turbulence and fi...
A series of fundamental problems related to jet engine air pollution and combustion were examined. T...
A viewgraph presentation describing experimental results and analytical developments about plume dia...
Idealized combustion model in which exothermic or endothermic reactions are permitted at or very nea...
The mathematical and physical basis of the SHIP computer program which embodies a finite-difference,...
The space station uses small rocket motors, called thrusters, for orientation control. Because of th...
Interacting two-phase flow in four differently sized pneumatic two-fluid atomizers was investigated ...
Chemical and chemical radiative effects on base flow field of multiple nozzled launch vehicles of Sa...
An investigation of oxygen compatibility and resistance to ignition of candidate materials for use i...
Modified P function applied to turbulent mixing of three coaxial, axisymmetric jets of reactive gase
Liquid propellant rocket engine performance computer program with distributed energy releas