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Flow Simulations for an Aft-Mounted Propfan Using Euler Equations
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English
Abstract
A new transonic flow analysis program based on the solution of Euler equations has been developed. The program is capable of analyzing the flow over a complete wing/body/tail/aft-mounted propfan configuration at arbitrary freestream conditions. Computed results for an advanced aft-mounted propfan configuration with and without propeller are reported in this paper.
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Yu, N., Kusunose, K., Chen, H., and Sommerfield, D., "Flow Simulations for an Aft-Mounted Propfan Using Euler Equations," SAE Technical Paper 861718, 1986, https://doi.org/10.4271/861718.Also In
References
- Yu, N. J. “Grid Generation and Transonic Flow Calculations for Three-Dimensional Configurations,” AIAA 80-1391 1980
- Sommerfield, D. M. Kusunose, K. Yu, N. J. “Computational Grid Generation for Complex Transport Configurations,” presented at 1st World Congress of Computational Mechanics Austin, TX September 1986
- Jameson, A. Baker, T. J. “Solution of the Euler Equations for Complex Configurations,” AIAA 83-1929 1983
- Leicher, S. “Analysis of Transonic and Supersonic Flows Around Wing-Body Combinations,” 14th ICAS Conference Proceedings Toulouse 157 167 September 9-14 1984
- Jain, R. K. Kroll, N. Radespiel, R. “Development of Efficient Algorithms for the Solutions of Full-Potential and Euler Equations on Vector Computers,” Notes on Numerical Fluid Mechanics Vieweg Verlag
- Thompson, J. F. “Numerical Grid Generation,” North Holland 1982
- Yu, N. J. Samant, S. S. Rubbert, P. E. “Flow Prediction for Propfan Configurations Using Euler Equations,” AIAA 84-1645 1984
- Yu, N. J. Chen, H. C. “Flow Simulations for Nacelle-Propeller Configurations Using Euler Equations,” AIAA 84-2143 1984
- Yu, N. J. Kusunose, K. Chen, H.C. Sommerfield, D.M. “Flow Simulations for a Complex Airplane Configuration Using Euler Equations,” AIAA 87-0454 presented at AIAA 25th Aerospace Sciences Meeting Reno, Nevada January 12-15 1987