A comparison between theoretical and experimental extinction behavior of composite solid propellants
Extinction model of composite solid propellant combustion including wall and flame heat release zones
Marxman, G. A.↗
Engineering topics
Marxman, G. A.
Publications and source records attributed to Marxman, G. A..
A theoretical and experimental study of propellant combustion phenomena during rapid depressurization Final report
Modified solid propellant combustion model for steady state analyses of burning rate and flame temperature
Kier, R. J.↗
Investigation of combustion instability in hybrid rockets Final report
Experimental and model studies of combustion instability in hybrid rocket propellants in pressure sensitive regime
Kier, R. J.↗
Nonlinear solid propellant burning rate behavior during abrupt pressure excursions.
Solid propellant burning rate behavior during abrupt environmental pressure excursions, using transient combustion model
Marxman, G. A.↗
A simple regression rate model for the pressure-sensitive domain of hybrid combustion.
Regression rate model for pressure sensitive hybrid combustion based on classical turbulent flame theory
Marxman, G. A.↗
Combustion instability and the role of chemical kinetics in hybrid combustion.
Combustion instability in hybrid rocket motors, noting chemical kinetics role and steady state regression rate
Marxman, G. A.↗
Effect of surface reactions on the solid propellant response function.
Surface coupled heat release effect on oscillatory amplitude of pressure coupled response in solid propellant
Marxman, G. A.↗
Propellant combustion phenomena during rapid depressurization Final report
Idealized combustion model in which exothermic or endothermic reactions are permitted at or very near solid-gas interfaces
Capener, E. L.↗
The effect of surface reactions on the solid propellant response function.
Surface coupled heat release effect on oscillatory amplitude of pressure coupled response in solid propellant
SOLID PROPELLANT↗
Boundary-layer combustion in propulsion.
Propulsion-oriented subsonic boundary layer combustion research, discussing turbulent and diffusion-limited conditions, radiant heat transfer, chemical kinetics and transient phenomena
RADIATIVE HEAT TRANSFER↗
Propellant combustion phenomenon during rapid depressurization Quarterly report no. 1, Jul. 1 - Sep. 30, 1965
Theoretical studies of processes occurring during rapid depressurization of burning solid propellants
PROPELLANT COMBUSTION↗