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A perspective on future directions in aerospace propulsion system simulationThe design and development of aircraft engines is a lengthy and costly process using today's methodology. This is due, in large measure, to the fact that present methods rely heavily on experimental testing to verify the operability, performance, and structural integrity of components and systems. The potential exists for achieving significant speedups in the propulsion development process through increased use of computational techniques for simulation, analysis, and optimization. This paper outlines the concept and technology requirements for a Numerical Propulsion Simulation System (NPSS) that would provide capabilities to do interactive, multidisciplinary simulations of complete propulsion systems. By combining high performance computing hardware and software with state-of-the-art propulsion system models, the NPSS will permit the rapid calculation, assessment, and optimization of subcomponent, component, and system performance, durability, reliability and weight-before committing to building hardware.
Document ID
19890012427
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miller, Brent A.
(NASA Lewis Research Center Cleveland, OH, United States)
Szuch, John R.
(NASA Lewis Research Center Cleveland, OH, United States)
Gaugler, Raymond E.
(NASA Lewis Research Center Cleveland, OH, United States)
Wood, Jerry R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-4608
NASA-TM-102038
NAS 1.15:102038
Meeting Information
Meeting: International Conference
Location: Santa Clara, CA
Country: United States
Start Date: April 30, 1989
End Date: May 5, 1989
Sponsors: International Supercomputing Inst.
Accession Number
89N21798
Funding Number(s)
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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