- Norris, Andrew
- August 2003.
- Physical Description:
- 1 electronic document
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- 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.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 20030068078. and 2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting; 89-99; NASA/TM-2003-211896.
- No Copyright.
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