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ablation absorption Aerospace Engineering AIAA angle atmosphere azimuthal boundary layer Bryson burning rate calculus of variations chamber pressure computed constant Control Theory decreases deflagration density downstream dp/dt dq/dt dynamic effect emission equation equilibrium experimental feedback Figure filter flat plate flow flux f free jet function gas phase grain surface guidance heat flux ignition initial integral ionosphere isothermal jet impingement Jour kinetic laminar laminar flow linear Mach number maximum mean sqaure measurements minimum fuel mixing region momentum flux nondimensional nozzle obtained occur optimal control performance index perturbation plasma plasma physics preheat q pressure decay pressure distribution pressure ratio problem psia radiation Reynold's number shadowgraph shown in Fig slot injection Solid Propellant splitter plate stagnation point stagnation pressure static pressure steady-state stream strong interaction subsonic supersonic temperature profile theoretical thermal thermocouple thrust turbulent University of Maryland variable wall jet Westronics