Location
Howard Johnson Plaza-Hotel, Columbia/ Atlantis Rooms
Start Date
27-4-1995 1:00 PM
End Date
27-4-1995 4:00 PM
Description
An efficient incompressible flow analysis code, INS3D, has been developed at NASA Ames Research Center and applied successfully to numerous aerospace applications. The INS3D code has also been applied to non-aerospace applications, such as biofluid problems, with great success. This paper presents a computational flow simulation capability originally developed for liquid rocket engine analysis and subsequently applied to analyze the left ventricular assist device being developed jointly by NASA Johnson Space Center and the Baylor College of Medicine.
Paper Session III-A - Dual-Use Applications of a Computational Fluid Dynamics Code for Viscous Incompressible Flow
Howard Johnson Plaza-Hotel, Columbia/ Atlantis Rooms
An efficient incompressible flow analysis code, INS3D, has been developed at NASA Ames Research Center and applied successfully to numerous aerospace applications. The INS3D code has also been applied to non-aerospace applications, such as biofluid problems, with great success. This paper presents a computational flow simulation capability originally developed for liquid rocket engine analysis and subsequently applied to analyze the left ventricular assist device being developed jointly by NASA Johnson Space Center and the Baylor College of Medicine.
Comments
Spin-Offs and Setbacks
Session Chairman: Paul Curto, Chief Technologist of the Inventions and Contributions Board (ICB), NASA Headquarters
Session Organizer: Suzanne Hodge