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Assessment of Stage 35 With APNASAAn assessment of APNASA was conducted at NASA Glenn Research Center under the Fundamental Aeronautics Program to determine their predictive capabilities. The geometry selected for this study was Stage 35 which is a single stage transonic compressor. A speedline at 100% speed was generated and compared to experimental data at 100% speed for two turbulence models. Performance of the stage at 100% speed and profiles of several key aerodynamic parameters are compared to the survey data downstream of the stator in this report. In addition, hub leakage was modeled and compared to solutions without leakage and the available experimental data.
Document ID
20120012587
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Celestina, Mark L. (NASA Glenn Research Center Cleveland, OH, United States)
Mulac, Richard (Toledo Univ. Cleveland, OH, United States)
Date Acquired
August 26, 2013
Publication Date
January 5, 2009
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
E-18238
Meeting Information
Meeting: AIAA 47th Aerospace Sciences Meeting
Location: Orlando, FL
Country: United States
Start Date: January 5, 2009
End Date: January 8, 2009
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581.02.08.03.21.03
Distribution Limits
Public
Copyright
Public Use Permitted.

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