Leading-Edge Shape and Aeroengine Fan Blade Performance-Reference-Cited by-同舟云学术

Leading-Edge Shape and Aeroengine Fan Blade Performance

Published:2003-05 Issue:3 Volume:19 Page:517-520
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Sayma A. I.¹,Kim M.¹,Smith N. H. S.²

Affiliation:

1. Imperial College, London, England SW7 2BX, United Kingdom

2. Rolls–Royce plc., Derby, England DE24 8BJ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.6137

Reference16 articles.

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2. Solid fuel ramjet simulator results - Experiment and analysis in cold flow

3. 3Ma, W. J. “Transpiration Cooling Phenomena in Separated Flow Field,” Ph.D. Dissertation, Dept. of Power Mechanical Engineering,National Tsing Hua Univ., Taiwan,June 2000.

4. Combustion in a turbulent mixing layer formed at a rearward-facing step

5. A stable and accurate convective modelling procedure based on quadratic upstream interpolation

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