Accession Number:

ADA024857

Title:

Flow Coefficients and Jet Deflection Angles for Combuster-Liner Entry Holes. Part II.

Descriptive Note:

Technical information series rept.,

Corporate Author:

GENERAL ELECTRIC CO SCHENECTADY N Y GENERAL ENGINEERING LAB

Personal Author(s):

Report Date:

1960-09-16

Pagination or Media Count:

42.0

Abstract:

Combustor liner cooling strips, oblong and square holes with trailing scoops were investigated and the performance determined. Also investigated were the effects on performance of multiple holes, main duct passage height, the flow angle pattern above an oblong hole, and scoop to hole area relationships.

Subject Categories:

  • Combustion and Ignition
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE