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Investigation of Turbines Suitable for Use in a Turbojet Engine Wtih High Compressor Pressure Ratio and Low Compressor-tip Speed V : Experimental Performance of Two-stage Turbine with Downstream StatorAn experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed that (1) at equivalent design work and speed the brake internal efficiency was 0.81 and the maximum efficiency obtained was 0.85, and (2) the downstream stator left very little energy in the form of tangential velocity in the gas and, in general, performed well with 0.78 recovery being obtained at equivalent design work and speed.
Document ID
19930089075
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Davison, Elmer H
Petrash, Donald A
Schum, Harold J
Date Acquired
August 16, 2013
Publication Date
October 21, 1951
Report/Patent Number
NACA-RM-E55H16
Accession Number
93R18365
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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