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- W2091511551 abstract "A technique for determining the thrust of a turbine engine during static testing is discussed. The technique relies upon inferring the local stream thrust from pitot pressure measurements. The local stream thrust can be spatially integrated to determine the total thrust. The influences of probe geometry and size on the thermochemistry of the probe flow field are addressed. The probe has a unique aerodynamic shape that automatically compensates for flow direction. This paper compares the fundamentals of both the standard scale force method and the “probe-based stream thrust” method of determining gross thrust. This paper also describes the validation of the probe technique against standard thrust stand data to be acquired during direct-connect static testing in Propulsion Development Test Cell J-1 at the U.S. Air Force Arnold Engineering Development Center (AEDC)." @default.
- W2091511551 created "2016-06-24" @default.
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- W2091511551 date "2004-06-21" @default.
- W2091511551 modified "2023-09-26" @default.
- W2091511551 title "Validation of Stream Thrust Probes for Direct-Connect Turbine Engine Testing" @default.
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- W2091511551 doi "https://doi.org/10.2514/6.2004-3547" @default.
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