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Comprehensive report of fan performance from duct rake instrumentation on 1.294 pressure ratio, 806 ft/sec tip speed turbofan simulator models
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Authors:
Jeracki, Robert J.
---
NASA Glenn Research Center.
Year: 2006 Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center,
Year: 2006 Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center,
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Abstract
Keywords
Pressure ratio. --- Scale models. --- Simulators. --- Tip speed. --- Turbofan engines. --- Ducted fans. --- Low speed wind tunnels. --- Wind tunnel tests.
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