TY  - JOUR
AB  - THE task of any recoil engine consists in transforming the chemical energy of fuel into the kinetic energy of gases leaving the nozzle. This article gives a brief survey of problems connected with transformations which the energy undergoes on the way from the fuel containers to the end of the nozzle. I have simplified as far as possible the problem, examining only the conditions in a rocket engine, without a gas turbine. Even in these simplified schemes the phenomena inside the combustion chamber and the nozzle are rather complicated and require careful examination.
VL  - 18
IS  - 3
SN  - 0002-2667
DO  - 10.1108/eb031347
UR  - https://doi.org/10.1108/eb031347
AU  - Bielkowicz P.
PY  - 1946
Y1  - 1946/01/01
TI  - Evolution of Energy in Jet and Rocket Propulsion
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 90
EP  - 92
Y2  - 2024/04/18
ER  -