Accession Number : AD0274925

Title :   FUNDAMENTALS OF HEAT TRANSFER IN AVIATION AND ROCKET ENGINEERING

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : AVDUYEVSKIY,V.S. ; DANILOV,YU.I.

Report Date : 26 APR 1962

Pagination or Media Count : 1

Abstract : Contents: Types of heat exchange, fundamental concepts and definitions Thermal conductivity under steady-state condi tions Convective heat exchange and fundamentals of theory of similarity Heat exchange with variation in aggregate state of matter Radiant heat exchange Theory and calculation of heat exchangers Thermal conductivity, non-stationary conditions Heat exchange at high velocities and high tem peratures of gas flow Heat exchange during chemical reactions in the boundary layer Hydrodynamic methods of firmly protective sur faces-Sweat cooling Barrier and combined cooling of combustion cham ber walls and nozzles in jet engines Film cooling of walls of combustion chamber and nozzles in liquid propellant rocket engines Concept of heat exchange in rarefied gases Some aspects of the calculation of the heat-up of winged flying craft; methods of thermal protection Some features of heat transfer calculation in liquid propellant rocket engines

Descriptors :   *HEAT TRANSFER, *ROCKET RESEARCH, HYDRODYNAMICS, LIQUID ROCKET PROPELLANTS, NUCLEAR POWER PLANTS, SWEAT COOLING, THERMAL CONDUCTIVITY

Distribution Statement : APPROVED FOR PUBLIC RELEASE