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Blood Pump Development Using Rocket Engine Flow Simulation TechnologyThis viewgraph presentation provides information on the transfer of rocket engine flow simulation technology to work involving the development of blood pumps. Details are offered regarding the design and requirements of mechanical heart assist devices, or VADs (ventricular assist device). There are various computational fluid dynamics issues involved in the visualization of flow in such devices, and these are highlighted and compared to those of rocket turbopumps.
Document ID
20020051212
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Kiris, Cetin C.
(NASA Ames Research Center Moffett Field, CA United States)
Kwak, Dochan
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Aerospace Medicine
Meeting Information
Meeting: UC Davis Applied Math Seminar Series
Location: Davis, CA
Country: United States
Start Date: March 4, 2002
Sponsors: California Univ.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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