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Computer program simplifies design of rotating components of turbomachineryDigital computer program performs stress analysis and burst speed calculations on rotating axisymmetric turbomachinery components. The computer printout contains the displacement of each nodal point, the stress at the center of each element, the average tangential stress within the component, and the burst speed.
Document ID
19670000235
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Lefevre, J. C.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Mathematics And Information Sciences
Report/Patent Number
NUC-10046
Accession Number
67B10235
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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