Accession Number:

AD0784015

Title:

Jet Cooling of the Leading Edge of a Turbine Blade,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1974-07-17

Pagination or Media Count:

9.0

Abstract:

One of the effective methods of the cooling of the leading edge of a turbine blade is jet blowing. In the reported experiments the object of the investigation was the model of a working blade made in a 51 scale with a chord of 60 mm. Parameters of the investigated system of jets were varied by means of an interchangeable nozzle part installed onto a permanent deflector.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE