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Visualization of flows in a motored rotary combustion engine using holographic interferometryThe use of holographic interferometry to view the small- and large-scale flow field structures in the combustion chamber of a motored Wankel engine assembly is described. In order that the flow patterns of interest could be observed, small quantities of helium were injected with the intake air. Variation of the air flow patterns with engine speed, helium flow rate, and rotor position are described. The air flow at two locations within the combustion chamber was examined using this technique.
Document ID
19860022111
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hicks, Y. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Schock, H. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Craig, J. E.
(Spectron Development Labs., Inc. Costa Mesa, Calif., United States)
Umstatter, H. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Lee, D. Y.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-88804
NAS 1.15:88804
AIAA PAPER 86-1557
E-3148
Report Number: NASA-TM-88804
Report Number: NAS 1.15:88804
Report Number: AIAA PAPER 86-1557
Report Number: E-3148
Meeting Information
Meeting: Joint Propulsion Conference
Location: Huntsville, AL
Country: United States
Start Date: June 16, 1986
End Date: June 18, 1986
Sponsors: AIAA, SAE, ASEE, ASME
Accession Number
86N31583
Funding Number(s)
PROJECT: RTOP 505-62-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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