Accession Number:

AD0762219

Title:

Rotor Blade of a Turbomachine,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1973-06-01

Pagination or Media Count:

5.0

Abstract:

The report describes various geometric configurations suggested for the root of a turbine blade in order to alleviate stress nonuniformity.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE