Engineering topics
Publications and source records attributed to Burstein, S. Z..
Computer program contains mathematical model which provides relationship between engine gas dynamics and combustion processes. Mathematically simulated explosions initiate gas disturbances. Design methods for damping disturbances can be studied to prevent future engine shutdown or destruction.
Mathematical models of nonlinear combustion instabilities in liquid propellant rocket engine
User manual for computer programs to determine high frequency instability in baffled annular liquid propellant rocket engines - Vol. 2
High frequency nonlinear combustion instability in baffled annular liquid propellant rocket engines - Vol. 1
Mathematical model and analysis of combustion processes in annular rocket engines for control of high amplitude combustion instability
Mathematical models and computer program on nonlinear combustion instability in liquid propellant rocket engines
Fluid dynamic pancake model and droplet evaporation and combustion analysis related to nonlinear combustion instability in liquid propellant rocket motors
Fluid dynamic model and diffusion-controlled flame analysis data on nonlinear combustion instability in liquid propellant rocket engines
Gas dynamic model for nonlinear combustion instability analysis in liquid propellant rocket engines
Hydrodynamic differential and difference equations and computer algorithm for nonlinear combustion instability in liquid propellant rocket engines, and Fortran IV listing
Model to determine vaporization rate of liquid fuel droplet
Aerothermochemical analysis of nonoscillatory and oscillatory characteristics of liquid bipropellant rocket motors - wave model, droplet heating, and evaporation computer program
Model and theoretical equations describing liquid propellant droplet ballistics and combustion gas behavior in bipropellant rocket motors - aerothermochemistry