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A new facility to study three dimensional viscous flow and rotor-stator interaction in turbinesA description of the Axial Flow Turbine Research Facility (AFTRF) being built at the Turbomachinery Laboratory of the Pennsylvania State University is presented. The purpose of the research to be performed in this facility is to obtain a better understanding of the rotor/stator interaction, three dimensional viscous flow field in nozzle and rotor blade passages, spanwise mixing and losses in these blade rows, transport of wake through rotor passage, and unsteady aerodynamics and heat transfer of rotor blade row. The experimental results will directly feed and support the analytical and the computational tool development. This large scale low speed facility is heavily instrumented with pressure and temperature probes and has provision for flow visualization and laser Doppler anemometer measurement. The facility design permits extensive use of the high frequency response instrumentation on the stationary vanes and more importantly on the rotating blades. Furthermore it facilitates detailed nozzle wake, rotor wake, and boundary layer surveys. The large size of the rig also has the advantage of operating at Reynolds numbers representative of the engine environment.
Document ID
19910015023
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lakshminarayana, B.
(Pennsylvania State Univ. University Park., United States)
Camci, C.
(Pennsylvania State Univ. University Park., United States)
Halliwell, I.
(General Electric Co. Cincinnati, OH., United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1989
Publication Information
Publication: NASA. Lewis Research Center, Structural Integrity and Durability of Reusable Space Propulsion Systems
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
91N24336
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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