Publication Date:
2019-07-12
Description:
Static tests on a segment of a transpiration-cooled turbine rotor blade with a wire-cloth shell were conducted to determine the flow coefficients associated with some representative metering orifices. Average flow coefficients from 0.96 to 0.79 were obtained for orifices of 0.031 to 0.102 inch diameter.
Keywords:
Aircraft Design, Testing and Performance
Type:
NACA-RM-E53L30a
Format:
application/pdf
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