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Experimental analysis of IMEP in a rotary combustion engineA real time indicated mean effective pressure measurement system is described which is used to judge proposed improvements in cycle efficiency of a rotary combustion engine. This is the first self-contained instrument that is capable of making real time measurements of IMEP in a rotary engine. Previous methods used require data recording and later processing using a digital computer. The unique features of this instrumentation include its ability to measure IMEP on a cycle by cycle, real time basis and the elimination of the need to differentiate volume function in real time. Measurements at two engine speeds (2000 and 3000 rpm) and a full range of loads are presented, although the instrument was designed to operate to speeds of 9000 rpm.
Document ID
19810007539
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schock, H. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Rice, W. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Meng, P. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-81662
E-680
Report Number: NASA-TM-81662
Report Number: E-680
Meeting Information
Meeting: Intern. Symp. of Automotive Engr.,
Location: Detroit, MI
Country: United States
Start Date: February 23, 1981
End Date: February 27, 1981
Accession Number
81N16054
Funding Number(s)
PROJECT: RTOP 505-41-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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