Accession Number:

ADA024316

Title:

Investigation of Slot Cooling for High-Speed Aircraft.

Descriptive Note:

Final rept. 1 Aug 71-30 Sep 75,

Corporate Author:

NEW YORK UNIV WESTBURY AEROSPACE AND ENERGETICS LAB

Personal Author(s):

Report Date:

1975-12-01

Pagination or Media Count:

23.0

Abstract:

Active film cooling for gas turbine blades has been investigated. Upstream injection at the leading edge and tangential injection downstream has been used to protect the blade.

Subject Categories:

  • Aircraft
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE