/rocket-nozzle

diverging nozzle purpose of this applet is to simulate the operation of a converging-diverging

Primary LanguageJupyter Notebook

rocket-nozzle

ɛ=area ratio =Ae/At

Mdot= rate of mass flow

Tc= chamber temperature

ɣ= gas constant of the fuel

R0=8.314

Vj= jet velocity of the fuel

image