The impact of computational zone interfacing on calculated scramjet performance
Author:
Affiliation:
1. USAF, Wright Laboratory, Wright-Patterson AFB, OH
2. Purdue University, West Lafayette, IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-390
Reference15 articles.
1. Dash, S. M., Sinha, N., Wolf, D. E., and York, B. J. "ComputationalModels for the Analysis/Design of Hypersonic Scramjet Components, Part I: Combustor and Nozzles Models, ', AIAA 86-1595,Huntsville AL, June 1986.
2. Moon, Y. J., Liou, M. "Conservative Treatment of Boundary Interfaces for Overlaid Grids and Multi-Level Grid Adaption," AIAA-89-198O-CP11989.
3. Conservative rezoning (remapping) for general quadrilateral meshes
4. Moon, Y. J. 'Numerical Study of Supersonic Combustor by Multi-block Grids with Mismatched Interfaces, AIAA-90-5204, Oct 90.
5. On Conservation at Grid Interfaces
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Elements of Pressure-Based Computational Algorithms for Complex Fluid Flow and Heat Transfer;Advances in Heat Transfer Volume 24;1994
2. REFERENCES;Computational Modeling for Fluid Flow and Interfacial Transport;1994
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