| || Non-Uniform Nozzle Flow Heat Exchange Effects
Author : Beri, J.N.
Source : Defence Science Journal ; Vol:15(2) ; 1965 ; pp 85-92
Subject : 536 Thermodynamics
Keywords : Stagnation Temperature ;Layer Effects;Heat Exchange
Abstract : Considering boundary layer effects in one-dimensional flow with heat exchange, true mean value flow parameters and their ratio to uniform free-stream values are derived. For one seventh power velocity distribution law and similar stagnation temperature and profiles variation in Mach number, stagnation temperature and impulse at the exit section are plotted versus boundary layer thickness.