3D Euler analysis of ducted propfan flowfields
Author:
Affiliation:
1. General Motors Corp., Allison Gas Turbines Div., Indianapolis, IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-3034
Reference21 articles.
1. Usab, W. J., Lee, A. K., and Sullivan, J. P. "A Comparison of Numerical Simulation and Experimental Measurements of Flow through Propellers", AIAA Paper 88-0367,1988.
2. Celestina, M. L., Mulac, R. A., and Adamczyk, J. J. "A Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller" ASME Paper 86-GT-136,1986.
3. Whitfield, D. L., Swafford,T.W., Janus,J. M., Mulac, R. A., and Belk, D. M. "Three-DimensionalUnsteady Euler Solutions for Propfans and Counter-Rotating Propfans in Transonic Flow", AIAA Paper 87-1197,1987.
4. Saito, S., Kobayashi, H., Nakamura, Y., and Matsuo, Y. "Predicted Flow Field Around the Advanced Propeller at Take-Off" AIAA Paper 88-3151,1988.
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1. 3-D viscous flow CFD analysis of the propeller effect on an advancedducted propeller subsonic inlet;29th Joint Propulsion Conference and Exhibit;1993-06-28
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