Back to Search Start Over

Computed and measured turbulence in axisymmetric reciprocating engines

Authors :
Grasso, F
Bracco, F. V
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

Subjects :
Aircraft Propulsion And Power

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