軸向穩定性 的英文怎麼說

中文拼音 [zhóuxiàngwěndìngxìng]
軸向穩定性 英文
axial stability
  • : 軸Ⅰ名詞1. (圓柱形的零件) axle; shaft 2. (對稱部分的直線) axis 3. (圓柱形的纏繞器物) roller; spool Ⅱ量詞(用於纏在軸上的線以及裝裱帶軸子的字畫)
  • : 形容詞1 (穩定; 穩當) steady; stable; firm 2 (穩重) steady; staid; sedate 3 (穩妥) sure; rel...
  • : Ⅰ形容詞1 (平靜; 穩定) calm; stable 2 (已經確定的; 不改變的) fixed; settled; established Ⅱ動詞...
  • : Ⅰ名詞1 (性格) nature; character; disposition 2 (性能; 性質) property; quality 3 (性別) sex ...
  • 穩定性 : antiwhip
  • 穩定 : 1 (使穩定) stabilize; steady 2 (穩固安定) stable; steady 3 (物質的性能不易改變的作用) stabi...
  1. Through developing the comprehensive experiment device with large - scale drum strength and stability, the stress - measuring experiments of various wall thickness of the normal drums of the cranes were performed. the law that the stress of the drums along the circumference and along the axis changes with the load increase of the wire ropes was studies for the first time

    通過研製全比尺大型捲筒強度、綜合試驗裝置,對起重機常用規格的捲筒進行了各種壁厚條件下的應力測量試驗,首次對捲筒體周應力隨鋼絲繩逐步加載過程變化的規律進行了研究,發現最大應力產生在鋼絲繩繞過后3 ~ 5圈截面處,該現象與理論分析結果也是符合的。
  2. Obtain these chief research achievements. ( 1 ) the method of hydraulic fracturing, kaiser effect experiment and the finite element numerical simulation computation results, the direction of maximum horizontal principal stress intersect the small - angle of tunnel axial line, it is favorable to the stability of tunnel peripheral rock ; according to the test rust of field stress - relief method, at the present time, zhe gu mount tunnel have n ' t access to high crustal stress site, maximum principal stress magnitude is 17mpa ~ 20mpa

    主要獲得以下研究成果: ( 1 )綜合水壓致裂法、室內巖石kaiser效應試驗和有限元數值模擬計算研究成果,最大水平主應力方與隧道洞線小角度相交,對隧道圍巖有利;根據現場應力解除法測試結果,目前鷓鴣山隧道尚未進入高地應力段,最大主應力量級為17mpa 20mpa 。
  3. In order to investigate the unsteady flow frequency domain performances of an axial flow compressor at different mass flow, rotating speed and blade row spacing, plus inlet flow distortion, and considering aerodynamic characteristics and stability of the compressor, the low speed research compressor ( lsc ) at college of energy and power in nuaa is used to carry out the experiment studies. a large amount of test data has been gained through dynamic pressure transducers embedded in the stator blades at the tip, middle and hub section, then fast fourier transform algorithm ( fft ) is applied to calculate the frequency data

    為探討流壓氣機在工作流量、工作轉速及動?靜葉排間距變化時的葉片排流場非常頻譜特變化規律,並耦合進氣畸變的影響,同時與壓氣機氣動能和氣動相關聯,作者利用南京航空航天大學能源與動力學院的低速大尺寸流壓氣機( lsc )試驗器,採取在靜子葉片表面埋入動態壓力傳感器的實驗方法,對葉尖、葉中和葉根三個截面的動態壓力進行了測量,獲得了大量的可靠的實驗數據。
  4. Influence of preload factor on the stability of three - lobe journal bearing

    預負荷系數對三油楔徑滑動的影響
  5. Nonlinear dynamic stability for elastic shaft - disc rotating system under the periodic axial load

    載荷激勵下彈轉子系統的非線動力分析
  6. The results show that there are two centers of occurrence of llsw respectively in dong bei and jiang nan ; the regional torrential rain over the yangtze river basin is closely associated with llsw during the major periods of heavy rainfall ; the diurnal variation of the number of occurrence in the middle and low reaches of the yangtze river is the strongest in china there are some significant differences between llj and nallsw in positive season, spatial variation, diurnal variation and field of pressure. by the way, the important effect of inertial stability on heavy rainfall with both low level south - westerly jet and high level northerly strong flow is analyzed theoretically. the results show that the existence of the maximum of inertial stability in the left font of the low level jet is favor of the accumulation of the moist thermal energy, and conditional symmetric instability or convective instability can be expected in this region

    另外,慣的作用以往不受重視,本文通過對西南低空急流左前方和高空偏北大風右後方的慣和對稱的理論分析和實例計算,表明慣在伴有高低空急流的暴雨中有重要意義,揭示了梅雨暴雨的一種新的高低空急流耦合機制:低空急流左前方慣度大值區的存在,有利於低層濕熱能量的積累,使低層傾斜對流的不發展更多期望于條件對稱不或對流不;高空偏北大風(西風急流)的存在,是其右後方(右側)出現對稱不的有利條件,高空相對容易出現干對稱不;慣的作用,使低層的傾斜對流更偏於垂直方,有利於對流發展,使高層的傾斜對流更偏於水平方,有利於高層輻散。
  7. In the model, johnson - cook strength is combined with gurson - tvergaard - needleman yield criteria, and random distribution of microvoids is used. results show that quasi - periodic axial fracture will appear, which obstructs the mirror current of the armature

    在給微孔洞的初始擾動時,計算結果解釋了鋁電樞表面將要形成的不,它導致了電樞外表面出現周期裂紋,阻礙了鏡像電流,使fcg損耗增加。
  8. Nonlinear buckling of imperfect sandwich cylinders with orthotropic faces under axial compression

    具有對稱初始缺陷的正交各夾層圓柱薄殼的非線分析
  9. Vibration and stability are investigated for an axially moving beam constrained by a pinned end and a fixed end

    摘要研究一端簡支一端固支運動梁的橫振動和
  10. For the first time, the solenoid collecting magnetic field optical transducing principle is presented in this paper, and it is proved that the way to measure current by polarized light encircling conductor and that by polarized light threading solenoid axes are equivalent

    為了解決aoct的長期運行問題,首次提出了「螺線管聚磁光學傳感原理」 ,證明了偏振光圍繞著無限長通電導體測量電流與偏振光通過通電螺線管的測量電流,在光學傳感測量電流的意義上是等價的。
  11. So, it is definitely different from other amb - ab. three aspects have been studied theoretically in this paper which were based on an analysis of a compliant multleaf journal self - acting air bearing, which are as follows : ( 1 ) a set of theoretical analysis method which include the development of. physical and mathematical model, the solution of governing equations and the prediction of static and dynamic performance of the foil gas bearing is proposed. the above theoretical analysis method provides a possibility for numerical analysis

    本文在分析懸臂型彈箔片徑動壓氣體承工作原理的基礎上,做了以下幾個方面的工作: ( 1 )建立了懸臂型彈箔片徑動壓氣體承的物理和數學模型,確立並求解了控制方程,得到了靜、動態能的分析方法,為數值分析懸臂型彈箔片徑動壓氣體承奠了基礎。
  12. ( 3 ) the effects of the bearing parameters on the bearing performance have been numerically analyzed using finite element method. a finite element formulation has been developed. the numerical analysis of finite element has been realized with matlab language

    ( 3 )用有限元法數值分析了懸臂型彈箔片徑動壓氣體承的結構參數和運轉參數對承靜動態能和的影響。
  13. Longitudinal stability and control of a coaxial type helicopter in hovering

    式直升機懸停縱和操縱分析
  14. Zno thin film is compact and smooth, while the average size of the fine uniform grains, most of them are c - axis oriented, is about 30 - 50nm. the average oxygen content of zno thin film is over 40at %. fitful - sputtering helps to improve the orientation and compact extent crystal grains, and to decrease internal stress

    Sem 、 xrd和edx檢測結果顯示zno薄膜具有很好的工藝, zno薄膜平整緻密,粒徑分佈均勻,晶粒平均尺寸為30 - 50nm ,主要沿c生長,平均氧含量超過40at % 。
  15. Nonlinear stability of balanced rotor due to the effect of ball bearing internal clearance

    考慮徑內間隙的滾動承平衡轉子系統的非線動力
  16. The system is composed of inverse - fourier - transform system, optic fiber sensor and high sensitivity ccd. its software system of signal acquisition and data processing used the platform of virtual instrument labview. we tested system stability and investigated latex particle size from 32nm to 123nm, several phenomenon below have been found : ( 1 ) the experiment result is consistent with the theoretical arithmetic result of the relation between particle size and normalization light scattering energy at the position of 7 ? and 35 ? angle

    組建了包括反傅立葉變換系統、光纖傳感器以及高靈敏度ccd的大角度側光散射信號探測系統,設計了基於虛擬儀器labview平臺的信號採集和數據處理軟體,對系統和顆粒尺寸從32納米- 123納米的微乳液顆粒球進行了測試研究,發現以下現象: ( 1 )在與光成7和35夾角的位置,歸一化的散射光能量與粒徑大小關系的實驗結果跟理論分析規律完全一致。
  17. Geometric nonlinear behaviors in large span cable - stayed bridges have been analyzed in this paper, which include the sag of inclined cable stays caused by their own dead weight ; the interaction of large bending and axial deformation in bending members ; and the large displacements effects. then analyzing theories and researching levels of geometric nonlinear problems of modern cable - stayed bridges have summarized. and methods of modeling cable - stayed bridges for nonlinear finite element analysis have been discussed, which are the equivalent modulus of elasticity, introducing stability functions and continuously modifying geometry of structure

    本文分析了大跨徑斜拉橋幾何非線的主要影響因素,包括斜拉索的垂度效應、彎矩與力組合效應和大變形效應,同時對目前斜拉橋幾何非線問題的分析理論和研究水平進行了綜述,相應討論了各非線影響因素的處理方法,即分別採用等效彈模量法、引入函數和實時修正結構的幾何位置。
  18. The transverse vibration and stability analysis of an axially moving membrane

    運動薄膜的橫振動和分析
  19. Abstract : concerning the models for discribing aerodynamic stability of axial flow compressor, the original model is one - dimensional, and it is reasonable for the onset of surge only. for the onset of rotating stall, there are just some two - dimensional models at published literatures. a three - dimensional aerodynamic of compressor has been presented in this paper. an aerodynamic stability model concerning radial disturbance of compressor is presented. the calculated results show that the occurrence of radial disturbance is related to the axial velocity disturbance, which has important effect on aerodynamic stability of compressor. the position of onset of stall, in blade tip or hub, is dependent upon the characteristics of blade element. the comparisons of calculated results predicted by 2d and 3d aerodynamic stability model have also been made in this paper

    文摘:流壓氣機的氣動模型,最初為一維模型,僅適用於描述喘振發作.對于旋轉失速發作,在公開文獻中有一些二維模型發表.本文提出了一類考慮壓氣機徑擾動對失速影響的新的氣動模型.計算結果表明壓氣機的擾動往往隨著徑擾動的產生,徑擾動的強度影響壓氣機的氣動,在葉尖還是葉根首先產生失速與壓氣機基元葉柵特密切相關.本文對流壓氣機二維和三維氣動模型的計算結果進行了對比分析
  20. Concerning the models for discribing aerodynamic stability of axial flow compressor, the original model is one - dimensional, and it is reasonable for the onset of surge only. for the onset of rotating stall, there are just some two - dimensional models at published literatures. a three - dimensional aerodynamic of compressor has been presented in this paper. an aerodynamic stability model concerning radial disturbance of compressor is presented. the calculated results show that the occurrence of radial disturbance is related to the axial velocity disturbance, which has important effect on aerodynamic stability of compressor. the position of onset of stall, in blade tip or hub, is dependent upon the characteristics of blade element. the comparisons of calculated results predicted by 2d and 3d aerodynamic stability model have also been made in this paper

    流壓氣機的氣動模型,最初為一維模型,僅適用於描述喘振發作.對于旋轉失速發作,在公開文獻中有一些二維模型發表.本文提出了一類考慮壓氣機徑擾動對失速影響的新的氣動模型.計算結果表明壓氣機的擾動往往隨著徑擾動的產生,徑擾動的強度影響壓氣機的氣動,在葉尖還是葉根首先產生失速與壓氣機基元葉柵特密切相關.本文對流壓氣機二維和三維氣動模型的計算結果進行了對比分析
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