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논문 : 초음속 WIDE-CHORD 팬 블레이드의 고 되풀이 피로수명평가

PAPERS : EVALUATION OF THE HIGH CYCLE FATIGUE LIFE FOR SUPERSONIC WIDE-CHORD FAN BLADE


초록

키워드

참고문헌

  1. J. Wennerstrom, 'Design of highly loaded axial-flow fans and compressors', Concepts ETI, Inc., 2000
  2. 김경수, 김승우, 김우형, '소형 가스터빈 엔진의 구조설계 및 시험평가', 한국항공우주학회지 25권, 5호, 1997
  3. A.V.Srinivasan, 'Flutter and Resonant Vibration Characteristics of Engine Blades', ASME Journal of Engineering for Gas Turbines and Power, Vol. 119, 1997, pp. 742 ~ 775 https://doi.org/10.1115/1.2817053
  4. Steven R. Manwaring, Douglas C. Rabe, Christopher B. Lorence and Aspi R. Wadia, 'Inlet distortion generated forced response of a low aspect ratio transonic fan', International Gas Turbine and Aeroengine Congress & Exhibition, Birmingham, UK, June 10-13, 1996
  5. J. G. Marshall and M. Imregun, 'An analysis of the aeroelastic behaviour of a typical fan-blade with emphasis on the flutter mechanism', International Gas Turbine and Aeroengine Congress & Exhibition, Birmingham, UK, June 10-13, 1996
  6. U. Haupt, D. Jin and M. Rautenberg, 'Prediction of Blade Vibration Stress in Centrifugal Compressors due to Engine Order Excitation', International Gas Turbine Congress, Yokohama, October 27th-November 1st, 1991
  7. A.L. Berne, M.K. Leontiev, 'Experimental Investigations of GTE Part & Components for Dynamic Strength', Russia