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Combustor Simulation (2003)

Norris, Andrew

In: CASI

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Publication Date: 2018-06-06

Description: The goal was to perform 3D simulation of GE90 combustor, as part of full turbofan engine simulation. Requirements of high fidelity as well as fast turn-around time require massively parallel code. National Combustion Code (NCC) was chosen for this task as supports up to 999 processors and includes state-of-the-art combustion models. Also required is ability to take inlet conditions from compressor code and give exit conditions to turbine code.

Keywords: Computer Programming and Software

Type: 2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting; 89-99; NASA/TM-2003-211896

Format: application/pdf

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