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TECH56技术计划即将结束 被引量:1

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作者 梁春华
出处 《航空发动机》 2004年第1期46-46,共1页 Aeroengine
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同被引文献8

  • 1Michael T T, Scott M J, et al. A probabilistic assessment of NASA ultra-efficient engine technologies for a large subsonic transport[C]. ASME Turbo Expo 2004, Vienna, Austria, June 14-17, 2004.
  • 2Michael T T, Scott M J. An updated assessment of NASA ultra-efficient engine technologies[C]. 17th International Symposium on Air Breathing Engines, Munich, Germany, September 4-9, 2005.
  • 3Baker N, Roh A. New environmental friendly aero engine core concepts [C]. 18th International Symposium on Air Breathing Engines, Beijing, China, September 2-7, 2007.
  • 4Korsia J J. VITAL-European R&D program for greener aero-engines[C]. 18th International Symposium on Air Breathing Engines, Beijing, China, September 2-7, 2007.
  • 5Came P M, Robinson C J. Centrifugal compressor design[J]. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 1999, 213(2): 139-155.
  • 6Johnsen I, Bullock R. Aerodynamic design of axial flow compressors[R]. Washington DC: NASA, 1965.
  • 7Koch C C, Smith L H. Loss sources and magnitudes in axial-flow compressors[J]. Journal of Engineering for Power, 1976, 98(3): 411-424.
  • 8Wisler D C. Loss reduction in axial flow compressors through low-speed model testing[J]. Journal of Engineering for Gas Turbines Power, 1985, 107(2): 354-363.

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