Accession Number:

AD0094052

Title:

GAS-TO-BLADE HEAT-TRANSFER COEFFICIENTS AND TURBINE HEAT-REJECTION RATES FOR A RANGE OF ONE-SPOOL COOLED-TURBINE ENGINE DESIGNS

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC

Personal Author(s):

Report Date:

1956-05-14

Pagination or Media Count:

35.0

Abstract:

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE