Combustor Diffuser Modeling Part VI: Validation with a Four Passage Diffuser Rig Data
Author:
Affiliation:
1. GE Aircraft Engines
2. EACoE
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4173
Reference13 articles.
1. An Experimental/Computational Study of Airflow in the Combustor–Diffuser System of a Gas Turbine for Power Generation
2. Nikjoo, M., and Mongia, H., 1999, "Predictions of Flows with Adverse Pressure Gradients", AIAA Paper 99-2817.
3. Mongia, Hukam C., 2004, "Perspective of Combustion Modeling for Gas Turbine Combustors", AIAAPaper 2004-0156.
4. Mongia, H., Hsiao, G., Burrus, D., Sreedhar, PSVS, Rao, A., and Naik, P., 2004, "Combustor Diffuser Modeling Part I: Inlet Profiles and 2-D Calculations", AIAAPaper 2004-4168.
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3. Combustor Diffuser Modeling Part V: Validation with a Three Passage Diffuser Rig Data;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26
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5. Combustor Diffuser Modeling Part II: Inlet Profiles & 3-D Calculations;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26
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