Rocket performance prediction techniqueAttention 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.-
Document ID
19750036446
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Morgenthaler, J. H.
Stepien, W. R. (Bell Aerospace Co. Buffalo, N.Y., United States)