Comparison of measurements and predictions of flow in a gas turbine engine fuel nozzle
Author:
Affiliation:
1. Pratt & Whitney, West Palm Beach, FL
2. Pratt & Whitney, East Hartford, CT
3. UT Research Center, East Hartford, CT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-331
Reference4 articles.
1. Ryder, R.C. "CORSAIR-CCD: The, Baseline Solver for the National Combustion Code0022, AIAAPaper 98-3853, 1998;
2. Numerical study of the turbulent flow past an airfoil with trailing edge separation
3. P ' '
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