Accession Number:

ADB805720

Title:

Cooling of Gas Turbines. 8 - Theoretical Temperature Distributions Through Gas Turbine with Special Blades and Cooling Fins on the Rim

Descriptive Note:

Research memo.

Corporate Author:

FLIGHT PROPULSION RESEARCH LAB CLEVELAND OH

Personal Author(s):

Report Date:

1948-02-17

Pagination or Media Count:

32.0

Abstract:

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE