The rate of generation of gaseous propellant is, of course, equal to the rate of consumption of solid material.
This category helps you to calculate the basic thermodynamics numerical related to pressure, entropy, efficiency etc., – WINGS OF AERO
The convective heat transfer coefficient is calculated using the Bartz equation The exhaust gas temperature is determined using estimated heat flux, internal wall temperature and heat transfer coefficient.
In heat transfer and fluid dynamics, the film temperature is an approximation to the temperature of a fluid inside a convection boundary layer
Specific impulse is a measure of how efficiently a reaction mass engine creates thrust. For engines whose reaction mass is only the fuel they carry, specific impulse is exactly proportional…
The propelling nozzle converts a gas turbine or gas generator into a jet engine. P The power is defined by typical gauge pressure and temperature values for a turbojet of 20 psi