Engineering topics
Publications and source records attributed to Quan, V..
Computer program calculates the inviscid one-dimensional equilibrium, frozen, and nonequilibrium nozzle expansion of propellant exhaust mixtures containing carbon, hydrogen, oxygen, nitrogen, fluorine, chlorine and either aluminum, beryllium, boron or lithium. This program performs calculations for conical nozzles only.
Computer program calculates the inviscid one-dimensional equilibrium, frozen, and nonequilibrium nozzle expansion of propellant exhaust mixtures containing these six elements - carbon, hydrogen, oxygen, nitrogen, fluorine, and chlorine plus either aluminum, beryllium, boron or lithium. This program will perform calculations for contoured and conical nozzles.
Flow of chemically reacting propellant exhaust mixture in barrier cooled axisymmetric rocket nozzle
Convergent-divergent nozzle flow field solution obtained in form of perturbation about one dimensional flow field
FORTRAN 4 programs for calculating inviscid, one-dimensional and axisymmetric nonequilibrium nozzle flow fields and improving analytical predictions of delivered specific impulse
Computer program for axisymmetric two-phase reacting gas nonequilibrium nozzle flows analysis
Uniform two-zone perfect gas expansions in convergent-divergent nozzles