EFFECTS OF SOUND ABSORBING WALL ON BLADE ROW FLUTTER AND SOUND GENERATION UNDER INTERACTION OF MULTIPLE BLADE ROWS
EFFECTS OF SOUND ABSORBING WALL ON BLADE ROW FLUTTER AND SOUND GENERATION UNDER INTERACTION OF MULTIPLE BLADE ROWS
批准号:
16560165
负责人:
NAMBA Masanobu
金额:
$2.3万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
2004
资助国家:
日本
项目状态:
已结题
起止时间:
2004 至 2006
中文摘要
点击翻译按钮获取中文摘要
英文摘要
An unsteady lifting surface theory was developed for a model of three blade-rows with vibrating blades, to account for the simultaneous effects of adjacent blade rows situated upstream and downstream. A program was coded to compute unsteady aerodynamic force and work on blades for specified frequency, inter-blade phase angle and other design parameters. The validity of the program was confirmed by making a comparison for a model condition between the results from the present program and those of CFD Euler code computation conducted by Professor K.C. Hall of Duke University. Both results were in complete agreement.Parametric studies were conducted to investigate the simultaneous influences of the upsteam and downstream neighboring blade rows on unsteady loading caused by blade vibration. The effects of two downstream blade rows and two-upstream blade rows are also investigated.It is a common understanding that interaction of stator vanes with oncoming rotor wakes is the primary source o … More f the fan tone noise of turbofan engines. A prediction scheme on the basis of genuine 3-dimensional lifting surface theory including the effect of mutual aeroacoustic interaction between the rotor and the stator was developed. The scheme was further modified into a hybrid scheme, which deals with vortical interaction of stator vanes with oncoming vortical wake disturbances from the upstream rotor on the basis of CFD technique and deals with aeroacoustic interaction of the two blade rows on the basis of the unsteady lifting surface theory. A computation program was coded to predict the generated sound power.The above models were further generalized to include the effect of the sound absorbing walls, and the comprehensive models were mathematically formulated.New findings are summarized as follows.(1) The simultaneous influence of the upstream and downstream blade rows can not be accounted for by a simple superposition of interactions between two blade rows. The effect of the next blade row but one is also substantial in the case of very short distances between blade rows.(2) The effect of the acoustic interaction between the rotor and the stator on the radiated sound power is very substantial. The effect heavily depends on the harmonic number of the blade passing frequency. Less
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二重反転環状翼列のフラッター解析
对转环形叶栅颤振分析
DOI:
--
发表时间:
2006
期刊:
日本航空宇宙学会論文集 54・634
影响因子:
--
作者:
[Y.Shinohara, K.Toda, M.Yamamoto, 西野竜平]
通讯作者:
西野竜平
Improved Hybrid Method of Predicting Fan Tone Noise
预测风扇音调噪声的改进混合方法
DOI:
--
发表时间:
2006
期刊:
Turbomachines : Aeroelasticity, Aeroacoustics and Unstead Aerodynamics, published by Torus Press
影响因子:
--
作者:
[M.Kimura, M.Takei, Y.Saito, A.Saima, 難波昌伸]
通讯作者:
難波昌伸
Flutter Analysis of Annular Cascades in Counter Rotation
反向旋转环形叶栅的颤振分析
DOI:
--
发表时间:
2004
期刊:
Proceedings of Asian Joint Conference on Propulsion and Power 2004
影响因子:
--
作者:
[Ryohei NISHINO, Masanobu NAMBA, 難波昌伸, 難波昌伸]
通讯作者:
難波昌伸
Unsteady Aerodynamic Force on Oscillating Blades Under Interaction of Three Blade-rows
三排叶片相互作用下摆动叶片的非定常气动力
DOI:
--
发表时间:
2006
期刊:
Turbomachines : Aeroelasticity, Aeroacoustics and Unsteady Aerodynamics, published by Torus Press
影响因子:
--
作者:
[TG Hwang, DH Doh, T Kobayashi, K Tanaka, M Takei, 梅田眞三郎, 難波昌伸]
通讯作者:
難波昌伸
Flutter Analysis of a Rotating Blade Row under Aerodynamic Interaction with a Neighboring Blade Row
旋转叶片列在与相邻叶片列气动相互作用下的颤振分析
DOI:
--
发表时间:
2005
期刊:
Proceedings of 43^<rd> AIAA Aerospace Science Meeting and Exhibit AIAA2005-19
影响因子:
--
作者:
[村松久巳, 足立将明, Shinzaburo Umeda, 児島忠倫 他, 村松 久巳, 難波昌伸]
通讯作者:
難波昌伸
共 7 条
EFFECTS OF NEIGHBORING BLADE ROW ON SUPERSONIC CASCADE FLUTTER
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批准号:13650964
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$2.62万
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财政年份:2001
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负责人:NAMBA Masanobu
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依托单位:
RESEARCH ON CHEMICAL REACTION ENHANCENMENT OF SUPERSONIC MIXING GAS FLOWS
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批准号:07405046
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项目类别:Grant-in-Aid for Scientific Research (A)
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资助金额:$24.83万
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财政年份:1995
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负责人:NAMBA Masanobu
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依托单位:
ACTIVE ACOUSTIC SUPPRESSION OF CASCADE FLUTTER BY MEANS OF ACTUATOR SURFACE ON THE DUCT WALL
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批准号:07555305
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项目类别:Grant-in-Aid for Scientific Research (A)
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资助金额:$3.97万
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财政年份:1995
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负责人:NAMBA Masanobu
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依托单位:
RESEARCH ON COMBINED CYCLE ENGINES FOR SUPER AND HYPERSONIC AEROSPACE PROPULSION
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批准号:06302061
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项目类别:Grant-in-Aid for Co-operative Research (A)
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资助金额:$13.95万
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财政年份:1994
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负责人:NAMBA Masanobu
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依托单位:
STEADY AND UNSTEADY AERODYNAMIC CHARACTERISTICS OF SUPERSONIC THROUGH-FLOW FAN CASCADE
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批准号:03452099
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项目类别:Grant-in-Aid for General Scientific Research (B)
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资助金额:$4.54万
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财政年份:1991
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负责人:NAMBA Masanobu
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依托单位:
STUDY OF THREE-DIMENSIONAL EFFECTS ON AEROELASTIC CHARACTERISTICS OF CASCADE
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批准号:61550048
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项目类别:Grant-in-Aid for General Scientific Research (C)
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资助金额:$1.41万
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财政年份:1986
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负责人:NAMBA Masanobu
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依托单位:
海外基金