Accession Number : AD0701351

Title :   HEAT TRANSFER PROBLEMS IN ADVANCED GAS TURBINES FOR NAVAL APPLICATION.

Descriptive Note : Technical rept.,

Corporate Author : MINNESOTA UNIV MINNEAPOLIS DEPT OF MECHANICAL ENGINEERING

Personal Author(s) : Eckert,Ernst R. G.

Report Date : 01 JAN 1970

Pagination or Media Count : 123

Abstract : Activities and accomplishments, up to date, are summarized which have been obtained in research on heat transfer problems in advanced gas turbines at the Heat Transfer Laboratory, School of Mechanical and Aerospace Engineering, University of Minnesota. The report discusses: Introduction; Flow and heat transfer in rotating cavities; Turbulence measurements in combustion gases; Film cooling analogy; Thermal radiation properties; Studies on turbulent shear layers; and flow through porous media. (Author)

Descriptors :   (*GAS TURBINES, *HEAT TRANSFER), STAGNATION POINT, TURBINE BLADES, THERMAL RADIATION, CENTRIFUGAL FIELDS, REYNOLDS NUMBER, JET MIXING FLOW, INTERACTIONS, FLUID MECHANICS

Subject Categories : Thermodynamics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE