Flow Coefficients and Jet Deflection Angles for Combuster-Liner Entry Holes. Part II.
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 16, 1960
- Accession Number
- ADA024857
Entities
People
- W. F. Venneman
Organizations
- General Electric