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Probabilistic Structural Analysis of SSME Turbopump Blades: Probabilistic Geometry EffectsA probabilistic study was initiated to evaluate the precisions of the geometric and material properties tolerances on the structural response of turbopump blades. To complete this study, a number of important probabilistic variables were identified which are conceived to affect the structural response of the blade. In addition, a methodology was developed to statistically quantify the influence of these probabilistic variables in an optimized way. The identified variables include random geometric and material properties perturbations, different loadings and a probabilistic combination of these loadings. Influences of these probabilistic variables are planned to be quantified by evaluating the blade structural response. Studies of the geometric perturbations were conducted for a flat plate geometry as well as for a space shuttle main engine blade geometry using a special purpose code which uses the finite element approach. Analyses indicate that the variances of the perturbations about given mean values have significant influence on the response.
Document ID
19850019646
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nagpal, V. K.
(Sverdrup Technology, Inc. Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1985
Publication Information
Publication: NASA. Lewis Research Center Struct. Integrity and Durability of Reusable Propulsion Systems
Subject Category
Structural Mechanics
Accession Number
85N27958
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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