كليدواژه هاي لاتين
Variable area nozzle, Convegent nozzle, Convergent-divergent (C-D) nozzle, Afterburner, Reverse thrust, Thrust vecturing, Back pressure, Area ratio, Gross thrust coefficient, Flow coefficient, Velocity coefficient, Angularity coefficient, Nozzle performance, fuel control, Flow unsteadiness, contraction ratio, Combustion chamber