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A Comparison Between Full and Simplified Navier-Stokes Equation Solutions for Rotating Blade Cascade Flow on S1Stream Surface of Revolution
1985
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
unpublished
A method for solving the Navier-Stokes equations of the rotating blade cascade flow on S1 stream surface of revolution is developed in the present paper. In this paper a complete set of full and simplified Navier-Stokes equations is given which includes stream-function equation, energy equation and entropy equation, equation of state for a perfect gas, formula for estimating density and formulas for calculating viscous forces, work done by viscous force, dissipation function and heat-transfer
doi:10.1115/85-gt-4
fatcat:3kk54grc4bhkta7df2lopna3zu