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Vibration computer programs E13101, E13102, E13104, and E13112 and application to the NERVA program. Project 187: Methodology documentationPrograms for the analyses of the free or forced, undamped vibrations of one or two elastically-coupled lumped parameter teams are presented. Bearing nonlinearities, casing and rotor distributed mass and elasticity, rotor imbalance, forcing functions, gyroscopic moments, rotary inertia, and shear and flexural deformations are all included in the system dynamics analysis. All bearings have nonlinear load displacement characteristics, the solution is achieved by iteration. Rotor imbalances allowed by such considerations as pilot tolerances and runouts as well as bearing clearances (allowing concail or cylindrical whirl) determine the forcing function magnitudes. The computer programs first obtain a solution wherein the bearings are treated as linear springs of given spring rates. Then, based upon the computed bearing reactions, new spring rates are predicted and another solution of the modified system is made. The iteration is continued until the changes to bearing spring rates and bearing reactions become negligibly small.
Document ID
19730015945
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mironenko, G.
(Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1972
Subject Category
Nuclear Engineering
Report/Patent Number
N8120R:72-038
NASA-CR-132220
Report Number: N8120R:72-038
Report Number: NASA-CR-132220
Accession Number
73N24672
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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