Flow Coefficients and Jet Deflection Angles for Combuster-Liner Entry Holes. Part II.
Technical information series rept.,
GENERAL ELECTRIC CO SCHENECTADY N Y GENERAL ENGINEERING LAB
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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.
- Combustion and Ignition
- Jet and Gas Turbine Engines