Accession Number:

ADA181558

Title:

Studies of Gas Turbine Heat Transfer Airfoil Surface and End-Wall.

Descriptive Note:

Annual progress rept. 28 Feb 86-1 Apr 87,

Corporate Author:

MINNESOTA UNIV MINNEAPOLIS DEPT OF MECHANICAL ENGINEERING

Report Date:

1987-04-01

Pagination or Media Count:

78.0

Abstract:

This report documents work on the topic of heat transfer from gas turbine airfoil, end-wall and internal passage surfaces. The research is divided into the following subtopics curvature effects, including transition and film cooling and airfoil heat transfer, including portions near the endwall. Keywords Cascade structures End-all curvature.

Subject Categories:

  • Jet and Gas Turbine Engines
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE