Accession Number:

AD0625242

Title:

THERMAL RESISTANCE OF TAIL CONNECTIONS OF TURBINE BLADES,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1965-11-30

Pagination or Media Count:

17.0

Abstract:

The report discusses a calculated determination of thermal resistance of tail sections of Lavals Y-shaped, arborescent type turbine blade.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE