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Fluid mechanics, acoustics, and design of turbomachinery, part 1A conference was conducted to analyze the effects of air flow on turbomachinery design. The subjects discussed are: (1) equations for compressible flow through turbomachines, (2) influence of axial velocity ratio on cascade performance, (3) three dimensional flow in transonic axial compressor blade rows, (4) prediction of turbulent shear layers in turbomachines, and (5) boundary layers in centrifugal compressors.
Document ID
19750003102
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Lakshminarayana, B. (Pennsylvania State Univ. University Park, PA, United States)
Britsch, W. R. (NASA Lewis Res. Center University Park, PA, United States)
Gearhart, W. S. (Pennsylvania State Univ.)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
LC-72-600087-PT-1
NASA-SP-304-PT-1
Accession Number
75N11174
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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