Probability characteristics for vibratory mode of detuned bladed disk assemblies

被引：0
|
作者：
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China [1 ]
机构：
来源：
Hangkong Dongli Xuebao | 2009年 / 9卷 / 2040-2045期
关键词：
10;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [31] AN INVESTIGATION OF DUAL MODE PHENOMENA IN A MISTUNED BLADED DISK
    STANGE, WA
    MACBAIN, JC
    JOURNAL OF VIBRATION ACOUSTICS STRESS AND RELIABILITY IN DESIGN-TRANSACTIONS OF THE ASME, 1983, 105 (03): : 402 - 407
  • [32] Reduced order models of rotating mistuned bladed disk assemblies using component mode synthesis methods with interface modes
    Duvauchelle, F.
    Tran, D. -M.
    PROCEEDINGS OF ISMA 2004: INTERNATIONAL CONFERENCE ON NOISE AND VIBRATION ENGINEERING, VOLS 1-8, 2005, : 2515 - 2523
  • [33] Experimental and Numerical Assessment of Mistuning Effects on Vibratory Response of a Bladed Disk With Underplatform Dampers
    Pourkiaee, S. Mehrdad
    Berruti, Teresa
    Zucca, Stefano
    Neuville, Geoffrey
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2021, 143 (03):
  • [34] EXPERIMENTAL AND NUMERICAL ASSESSMENT OF MISTUNING EFFECTS ON VIBRATORY RESPONSE OF A BLADED DISK WITH UNDERPLATFORM DAMPERS
    Pourkiaee, S. Mehrdad
    Berruti, Teresa
    Zucca, Stefano
    Neuville, Geoffrey
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 11, 2020,
  • [35] Research on vibration problem of integral mistuned bladed disk assemblies at home and abroad
    Bai, B. (baibin@126.com), 1600, Beijing University of Aeronautics and Astronautics (BUAA) (29):
  • [36] Robustness Analysis of Intentional Mistuning Patterns in Randomly Mistuned Bladed Disk Assemblies
    Yumer, M. E.
    Cigeroglu, E.
    Ozguven, H. N.
    PROCEEDINGS OF ISMA2010 - INTERNATIONAL CONFERENCE ON NOISE AND VIBRATION ENGINEERING INCLUDING USD2010, 2010, : 4865 - 4874
  • [37] Equivalent Linearization of Bladed Disk Assemblies With Friction Nonlinearities Under Random Excitation
    Foerster, Alwin
    Panning-von Scheidt, Lars
    Wallaschek, Joerg
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2021, 143 (05):
  • [38] Reduced order modeling and vibration analysis of mistuned bladed disk assemblies with shrouds
    Bladh, R
    Castanier, MP
    Pierre, C
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1999, 121 (03): : 515 - 522
  • [39] EQUIVALENT LINEARIZATION OF BLADED DISK ASSEMBLIES WITH FRICTION NONLINEARITIES UNDER RANDOM EXCITATION
    Foerster, Alwin
    Panning-von Scheidt, Lars
    Wallaschek, Joerg
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 11, 2020,
  • [40] NON-LINEAR FORCED RESPONSE ANALYSIS OF MISTUNED BLADED DISK ASSEMBLIES
    Yumer, M. Ersin
    Cigeroglu, Ender
    Ozguven, H. Nevzat
    PROCEEDINGS OF THE ASME TURBO EXPO 2010, VOL 6, PTS A AND B, 2010, : 757 - 766
12345