CASE 9.1
Swirling flow in a model combustor with heat release.

Coordinator: Dr. S. Jakirlic, Darmstadt University of Technology

Schematic of the swirling flow in a model combuster	Typical Streamlines
Test Case Geometry	Axial Velocity

Please contact responsible coordinator for more computational details

References:

1. Pierce, Moin: LES of a confined coaxial jet with swirl and heat release, AIAA Paper 98-2892, 1998
   
2. Roback, Johnson: Mass and momentum turbulent transport experiments with confined swirling coaxial jets, NASA Contractor Rep. 168252, 1983
   
3. Lin: Modeling a Confined Swirling Coaxial Jet, Ann. Research Briefs, Center for Turbulence Research, Stanford University, Stanford, pp. 211-219 (downloadable from http://ctr.stanford.edu), 1998
   
4. Pierce, Moin: Method of Generating Equilibrium Swirling Inflow Conditions, AIAA Journal, Vol. 36, No. 7, pp. 1325-1327 , 1998
   
5. Wennerberg, Obi: Prediction of Strongly Swirling Flows in Quarl Expansions with a Non-Orthogonal Finite-Volume Method and a Second-Moment Turbulence Closure, Engineering Turbulence Modeling and Experiments, Vol. 2, pp. 197-206 , 1993
   
6. Wennerberg: Entwicklung eines vorhersagefähigen Berechnungsmodell für stark verdrallte Strömung mit Verbrennung, PhD Thesis, University of Erlangen-Nuremberg, Germany , 1995