Back to Search
Start Over
Computed and measured turbulence in axisymmetric reciprocating engines
- Source :
- AIAA Journal. 21
- Publication Year :
- 1983
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1983.
-
Abstract
- The turbulent flowfield of a spark-ignition engine affects strongly the combustion characteristics of the engine. The flowfield depends on the design of the combustion chamber and the intake system. The present investigation is concerned with the effect of chamber design, and engine operating conditions on top dead center turbulence prior to ignition. It is shown that many of the trends which were identified in earlier studies can be obtained from a single model. The employed model takes into account a two-dimensional axisymmetric flowfield. Attention is given to governing equations, boundary and initial conditions, a comparison of the computed results with measurements, and the effect of swirl and squish.
- Subjects :
- Aircraft Propulsion And Power
Subjects
Details
- Language :
- English
- Volume :
- 21
- Database :
- NASA Technical Reports
- Journal :
- AIAA Journal
- Notes :
- NAG3-8, , DE-AC04-81AL-16338
- Publication Type :
- Report
- Accession number :
- edsnas.19830043451
- Document Type :
- Report