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End wall flows in rotors and stators of a single stage compressorA computer code for solving the parabolized Navier-Stokes equations for internal flows was developed. Oscillations that develop in the calculation procedure are discussed. The measurements made in the hub and annulus wall boundary layers are summarized. The flow in the hub wall boundary layer, starting ahead of the inlet guide vanes to the inlet of the rotor is traced.
Document ID
19830008407
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Govindan, T. R. (Pennsylvania State Univ. University Park, PA, United States)
Murthy, K. N. S. (Pennsylvania State Univ. University Park, PA, United States)
Lakshminarayana, B. (Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
PSU/TURBO-83-2
NASA-CR-169800
NAS 1.26:169800
Report Number: PSU/TURBO-83-2
Report Number: NASA-CR-169800
Report Number: NAS 1.26:169800
Accession Number
83N16678
Funding Number(s)
CONTRACT_GRANT: NSG-3212
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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