NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
TurbomachineryThe discipline research in turbomachinery, which is directed toward building the tools needed to understand such a complex flow phenomenon, is based on the fact that flow in turbomachinery is fundamentally unsteady or time dependent. Success in building a reliable inventory of analytic and experimental tools will depend on how the time and time-averages are treated, as well as on who the space and space-averages are treated. The raw tools at disposal (both experimentally and computational) are truly powerful and their numbers are growing at a staggering pace. As a result of this power, a case can be made that a situation exists where information is outstripping understanding. The challenge is to develop a set of computational and experimental tools which genuinely increase understanding of the fluid flow and heat transfer in a turbomachine. Viewgraphs outline a philosophy based on working on a stairstep hierarchy of mathematical and experimental complexity to build a system of tools, which enable one to aggressively design the turbomachinery of the next century. Examples of the types of computational and experimental tools under current development at Lewis, with progress to date, are examined. The examples include work in both the time-resolved and time-averaged domains. Finally, an attempt is made to identify the proper place for Lewis in this continuum of research.
Document ID
19880006410
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Simoneau, Robert J.
(NASA Lewis Research Center Cleveland, OH, United States)
Strazisar, Anthony J.
(NASA Lewis Research Center Cleveland, OH, United States)
Sockol, Peter M.
(NASA Lewis Research Center Cleveland, OH, United States)
Reid, Lonnie
(NASA Lewis Research Center Cleveland, OH, United States)
Adamczyk, John J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1987
Publication Information
Publication: Aeropropulsion '87. Session 3: Internal Fluid Mechanics Research
Subject Category
Aircraft Propulsion And Power
Accession Number
88N15792
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available