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Rotary engine performance computer program (RCEMAP and RCEMAPPC): User's guideThis report is a user's guide for a computer code that simulates the performance of several rotary combustion engine configurations. It is intended to assist prospective users in getting started with RCEMAP and/or RCEMAPPC. RCEMAP (Rotary Combustion Engine performance MAP generating code) is the mainframe version, while RCEMAPPC is a simplified subset designed for the personal computer, or PC, environment. Both versions are based on an open, zero-dimensional combustion system model for the prediction of instantaneous pressures, temperature, chemical composition and other in-chamber thermodynamic properties. Both versions predict overall engine performance and thermal characteristics, including bmep, bsfc, exhaust gas temperature, average material temperatures, and turbocharger operating conditions. Required inputs include engine geometry, materials, constants for use in the combustion heat release model, and turbomachinery maps. Illustrative examples and sample input files for both versions are included.
Document ID
19940010719
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bartrand, Timothy A.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Willis, Edward A.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1993
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-191192
E-8133
NAS 1.26:191192
Report Number: NASA-CR-191192
Report Number: E-8133
Report Number: NAS 1.26:191192
Accession Number
94N15192
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
PROJECT: RTOP 505-62-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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