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二元翼型水滴收集率计算研究 被引量:1

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出处 《民用飞机设计与研究》 2008年第2期15-18,33,共5页 Civil Aircraft Design & Research
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  • 1DOT/FAA/AR. Report of the 12A working group on determination of critical ice shapes for the certification of aircraft[R]. DOT/FAA /AR-00/37, 2000.
  • 2Bragg M B, Broeren A P, Blumenthal L A. Iced-airfoil aerodynamics[J]. Progress in Aerospace Sciences, 2005, 41: 323-362.
  • 3Papadakis Michael, Yeong Hsiung-Wei, Wong See-Cheuk. Aerodynamic performance of a swept wing with ice accretion[C]. 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, 2003: 1-48.
  • 4Jaiwon Shin, Brian Berkowitzt, Hsun H, et al. Prediction of ice shapes and their effect on airfoil drag[J]. Journal of Aircraft, 1994, 31(2): 263-270.
  • 5CCAR-25-R4运输类飞机适航标准[S]. 中国民用航空规章, 2011.
  • 6AC25.1419. Certification of transport category airplanes for flight in icing conditions[S]. Advisory Circular, 1999.
  • 7AC25-25. Performance and handling characteristics in the icing conditions specified in part 25, Appendix C[S]. Advisory Circular, 2007.
  • 8Mingione G, Brandi V. Ice accretion prediction on multielements airfoils[J]. Journal of Aircraft, 1998, 35(2): 1-11.
  • 9Myers T G, Charpin J P F. A mathematical model for atmospheric ice accretion and water flow on a cold surface[J]. International Journal of Heat and Mass Transfer, 2004,47: 5483-5500.
  • 10Fortin G, Ilinca A, Laforte J, et al. New roughness computation method and geometric accretion model for airfoil icing[J]. Journal of Aircraft, 2004, 41(1): 119-127.

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