Accession Number : AD0783927
Title : Solutions to the Direct Problem of Heat Transfer between a Cooled Turbine Blade and Gas using the Dispersion Method,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Topunov,A. M. ; Iosifov,R. D. ; Rodionov,N. G.
Report Date : 24 JUL 1974
Pagination or Media Count : 12
Abstract : The dispersion method is used to solve a differential equation of the third order describing heat exchange between gas and a cooled turbine blade.
Descriptors : *Gas turbine blades, *Heat transfer, Differential equations, Air cooled, Translations, USSR
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE