Problems of Heat Transfer in Gas Turbines (Collection of Articles)

Abstract

The articles in this collection contain the results of theoretical and experimental studies of heat transfer in gas turbines, and the temperature states of turbine blades, disks, and rotors. Analysis is given of the boundary conditions formulated when stating problems of thermal conductivity relative to gas turbines. Results are given of a generalization of criterial formulas for calculating the heat-transfer coefficient in vane cascades. Certain specific problems of thermal conductivity are solved in general form and numerically for cooled hollow blades and disks.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Aug 30, 1972
Accession Number
AD0751513

Entities

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Birds
  • Blades
  • Boundary Layer
  • Computational Science
  • Differential Equations
  • Fluid Flow
  • Gas Flow
  • Gas Turbine Rotors
  • Gas Turbines
  • Heat Energy
  • Heat Transfer
  • Heat Transfer Coefficients
  • Hydrodynamics
  • Temperature Gradients
  • Thermal Conductivity
  • Two Dimensional

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerodynamics.
  • Combustion and Flow Dynamics.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)