Due to CFD Shortfalls, experimental data on gas turbine combustors is required to obtain insight into the combustion and flow mechanisms as well as for simulation and model validation and evaluation. The temperature and velocity fields of a generic can-type gas turbine combustor are presented for this purpose
Reference:
Meyers, BC, Mahmood, GI and Meyer, JP. 2009. Overview of experimental measurements in a generic can-type gas turbine combustor. International Aerospace Symposium of South Africa 2009 - Aerospace Technology: Enhancing our Partnerships. Leriba Lodge, Centurion, South Africa. 23rd - 25th November 2009, pp 23
Meyers, B., Mahmood, G., & Meyers, B. C. (2009). Overview of experimental measurements in a generic can-type gas turbine combustor. http://hdl.handle.net/10204/3926
Meyers, BC, GI Mahmood, and Bronwyn C Meyers. "Overview of experimental measurements in a generic can-type gas turbine combustor." (2009): http://hdl.handle.net/10204/3926
Meyers B, Mahmood G, Meyers BC, Overview of experimental measurements in a generic can-type gas turbine combustor; 2009. http://hdl.handle.net/10204/3926 .
International Aerospace Symposium of South Africa 2009 - Aerospace Technology: Enhancing our Partnerships. Leriba Lodge, Centurion, South Africa. 23rd - 25th November 2009
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