NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Performance of a supercharged direct-injection stratified-charge rotary combustion engineA zero-dimensional thermodynamic performance computer model for direct-injection stratified-charge rotary combustion engines was modified and run for a single rotor supercharged engine. Operating conditions for the computer runs were a single boost pressure and a matrix of speeds, loads and engine materials. A representative engine map is presented showing the predicted range of efficient operation. After discussion of the engine map, a number of engine features are analyzed individually. These features are: heat transfer and the influence insulating materials have on engine performance and exhaust energy; intake manifold pressure oscillations and interactions with the combustion chamber; and performance losses and seal friction. Finally, code running times and convergence data are presented.
Document ID
19900016666
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bartrand, Timothy A.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Willis, Edward A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-103105
NAS 1.15:103105
E-5430
Report Number: NASA-TM-103105
Report Number: NAS 1.15:103105
Report Number: E-5430
Meeting Information
Meeting: Joint Symposium on General Aviation Systems
Location: Ocean City, NJ
Country: United States
Start Date: April 11, 1990
End Date: April 12, 1990
Sponsors: FAA, AIAA
Accession Number
90N25982
Funding Number(s)
PROJECT: RTOP 505-62-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available