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Thermo-Mechanical Modeling and Analysis for Turbopump AssembliesLife, reliability, and cost are strongly impacted by steady and transient thermo-mechanical effect. Design cycle can suffer big setbacks when working a transient stress/deflection issue. Balance between objectives and constrains is always difficult. Requires assembly-level analysis early in the design cycle.
Document ID
20030068124
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Platt, Mike (Concepts NREC White River Jct., VT, United States)
Marsh, Matt (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
July 15, 2003
Subject Category
Mechanical Engineering
Meeting Information
Meeting: 14th Annual Thermal and Fluids Analysis Workshop
Location: Hampton, VA
Country: United States
Start Date: August 18, 2003
End Date: August 22, 2003
Funding Number(s)
CONTRACT_GRANT: NAS8-02019
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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