NASA NTRS · 19750036446
Rocket performance prediction technique
Abstract
Attention is given to a semiempirical correlation technique based on the rational assumption that the turbulent mixing of reactants is the rate controlling process in combustors employing diffusion flames. Questions of performance computation are considered along with the flow conditions. Predictions of combustion efficiency are obtained with the aid of a standard finite-difference computational technique.-
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Morgenthaler, J. H., Stepien, W. R.. 1974-09-01. Rocket performance prediction technique. https://ntrs.nasa.gov/citations/19750036446
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