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The engine design engine. A clustered computer platform for the aerodynamic inverse design and analysis of a full engineAn application for parallel computation on a combined cluster of powerful workstations and supercomputers was developed. A Parallel Virtual Machine (PVM) is used as message passage language on a macro-tasking parallelization of the Aerodynamic Inverse Design and Analysis for a Full Engine computer code. The heterogeneous nature of the cluster is perfectly handled by the controlling host machine. Communication is established via Ethernet with the TCP/IP protocol over an open network. A reasonable overhead is imposed for internode communication, rendering an efficient utilization of the engaged processors. Perhaps one of the most interesting features of the system is its versatile nature, that permits the usage of the computational resources available that are experiencing less use at a given point in time.
Document ID
19930002035
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sanz, J.
(NASA Lewis Research Center Cleveland, OH, United States)
Pischel, K.
(NASA Lewis Research Center Cleveland, OH, United States)
Hubler, D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
E-7278
NAS 1.15:105838
NASA-TM-105838
Report Number: E-7278
Report Number: NAS 1.15:105838
Report Number: NASA-TM-105838
Meeting Information
Meeting: Grand Challenges
Location: Washington, DC
Country: United States
Start Date: September 20, 1992
End Date: September 22, 1992
Sponsors: NRL
Accession Number
93N11223
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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