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Coupled Fluid and Structural Analysis of Pump Stages for Space Propulsion SystemsThe objective is to develop a coupled fluid/structure analysis tool for rocket turbopumps, advance hardware concepts and designs, and improve safety, reliability, and cost of space transportation.
Document ID
20030068079
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Hah, Chunill (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2003
Publication Information
Publication: 2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting
Subject Category
Aircraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20030068074Collected Works2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting20030068074Collected Works2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting
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