The Evolution of Energy in Jet and Rocket Propulsion

Abstract

IT is now possible to determine the temperature in the combustion chamber with greater accuracy than in Part V. However, to simplify the problem it is necessary to make a number of far‐going assumptions. A more detailed survey of phenomena occurring in the combustion chamber will be given in a later Part; at present we are merely enumerating the simplified schemes, which enable us to tackle the problem.

Citation

Bielkowicz, P. (1946), "The Evolution of Energy in Jet and Rocket Propulsion", Aircraft Engineering and Aerospace Technology, Vol. 18 No. 6, pp. 206-208. https://doi.org/10.1108/eb031382