The Evolution of Energy in Jet and Rocket Propulsion
Aircraft Engineering and Aerospace Technology
Article publication date: 1 June 1946
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.
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
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