氣流中的擾動 的英文怎麼說

中文拼音 [liúzhōngderǎodòng]
氣流中的擾動 英文
imperfections in flows
  • : Ⅰ名詞1 (氣體) gas 2 (空氣) air 3 (氣息) breath 4 (自然界冷熱陰晴等現象) weather 5 (氣味...
  • : Ⅰ動1 (液體移動; 流動) flow 2 (移動不定) drift; move; wander 3 (流傳; 傳播) spread 4 (向壞...
  • : 4次方是 The fourth power of 2 is direction
  • : Ⅰ動詞1 (擾亂; 攪擾) harass; trouble 2 (客套話 因受人款待而表示客氣) trespass on sb s hospital...
  • 氣流 : 1 [氣象學] air current; airflow; wind current; airstream2 [語言學] breath氣流紡紗 open end spinni...
  • 擾動 : excitation; turbulent motion; turbulence; destabilization; [物理學] perturbation motion; [地質學]...
  1. According to their space position, the seismic features of shallow gas in this region can be divided into three groups : ( 1 ) features in the stratum : acoustic blanket, acoustic curtains, acoustic turbidity, irregular strong top reflection boundary, and phase pull - down in both flanks ; ( 2 ) features of the seabed : seabed pockmark and giant sunken pit ; ( 3 ) features in the seawater column : acoustic plumes, cloudy turbidity and point - line - type reflection

    該區淺層地震特徵按空間位置分為3大類: ( 1 )地層特徵:聲學空白、聲學幕、聲學、不規則強反射頂界面、兩側相位下拉; ( 2 )海底面特徵:海底麻坑、大型塌陷坑; ( 3 )海水層特徵:聲學羽、雲狀、點劃線反射。
  2. Firstly, a representative wind and wave model, which could both simulate the main characteristics of wig over sea waves and be suitable for numerical calculation, is presented. the model completely considers the fully nonlinear effect of wave surface on the wavy air flow, separates the disturbance of wave surface from the wing - air wave interaction flow, and overcomes the numerical calculation difficulties due to the large difference of dimensions between wing and water waves

    首先針對機翼在風浪非定常非線性力問題,提出了一個既能夠反映風浪場主要特徵又適合於數值計算風浪場模型,該模型完整地考慮了波浪表面對全非線性影響,使波面對分離出來,消除了機翼和波浪幾何尺度上巨大差異帶來數值計算上困難。
  3. It is studied that the formation mechanism of taylor bubble and its control method in gas - liquid two - phase flow, which affects the pressure balance and mechanical driving efficiency in the flow of petroleum engineering. experiments show that the formation of taylor bubble in gas - liquid two - phase flow is due to the intensive congregation and amalgamation of small bubbles driven by void fraction waves and that the highly turbulent flow is able to restrain this formation. thus, the flow regime transition may be checked by increasing the flow turbulence and controlling the disturbed frequency

    對大管徑-液兩相嚴重影響壓力平衡與機械驅效率段塞生成機制和控制方法進行了研究,實驗證明段塞形成是由於空隙率波大幅度增長使泡高度集,並形成聚並所致。強湍可以抑制taylor泡形成。因此,通過強化湍或控制頻率可以對泡聚並起明顯抑制作用。
  4. It is necessary to study the unsteady nonlinear aerodynamic characteristics of a wig flying in air with disturbed waves for the design of high - performance wig vehicle, especially for the subject that how to improve the safety, maneuver ability near sea wave, and economics of the wig flying over sea waves

    研究地效翼在風浪掠海飛行非定常力問題,對于高性能地效翼船設計,特別是對于提高地效翼船在風浪飛行安全性,操縱性以及經濟性都是十分重要
  5. The flight control system of attack helicopter and the influence of disturbance during noe flight are studied in this dissertation. and the use of h robust control and dynamic inversion schemes in flight control system are discussed

    本文主要對貼地飛行時武裝直升機飛行控制系統進行深入研究和探索,討論了貼地飛行時對直升機系統影響,研究了h _魯棒控制和態逆控制在直升機飛控系統應用。
  6. The results of numerical experiments, using the four - dimensional variational data assimilation system of the nonhydrostatic mesoscale model mm5, show that : the tangent linear model and adjoint model conducted by keeping the " on - off " switches the same as the basic state, can provide a good approximation of the first - order information to the nlm perturbation and a good descent direction for the minimization procedure ; switching on and off at every other time step in the kuo cumulus parameterization scheme do n ' t impact the convergence rate of cost function ; the existence of the switches do n ' t impact improvement to the mm5 model rainfall prediction because that not only specific humidity, but also wind, temperature and pressure are assimilated into the model

    非靜力尺度數值模式mm5四維變分資料同化系統進行數值試驗結果表明: 「開關」變量保持與基態一致,所構造切向線性模式能夠提供關于非線性模式一階近似,伴隨模式所計算梯度值能夠為最小化過程提供較好下降方向;郭氏降水參數化方案每隔一個積分步交替發生並不影響目標函數最小化收斂速度; 「開關」變量存在也不影響將風、溫度、壓和比濕結合起來同化對mm5降水預報準確性提高。
  7. The flow propagates northward and marches across the equation, then passes through the trough of summer monsoon over south china sea and finally gets to the yangtze river valley, which sequentially effect the southwest airflow of the west side of subtropical high

    ( 3 )在副高西伸過程,南半球澳大利亞高壓北側冷空向北推進,經向風持續向北傳播,從而影響副高西側偏南
  8. From time to time, under the influence of upper air disturbances, cold air from this anticyclone plunges southward through china and brings outbursts of cold air to the south china coastal areas

    有時,在高空影響下,冷空會南下橫過國。這些冬季季候風寒潮,最後為華南沿岸帶來一陣陣冷空
  9. The paper introduces the basic principle of the inducement type ventilation in the province of aerodynamics : disturbed characteristic of high - speed cascade can effectively leads quiescent air around it and drive air flow, compares and analyzes the traditional ventilation type and inducement ventilation type applied in underground garage in the facets of airflow organization, practicability and economy, coming to the conclusion that the inducement type ventilation is applied to the underground garage in the facets of economy, practicality and high efficiency

    摘要介紹了誘導式通風利用空力學高速噴特性,能夠有效地誘導周圍靜止,帶基本工作原理,就傳統通風方式和誘導通風方式,在地下車庫應用組織、實用性、經濟性等幾個方面做了比較,分析認為,誘導式通風因其經濟、適用、高效特性適合在地下車庫應用。
  10. Under the influence of the submergence the turbulence intensity are quite high at the end stage of burning. however, the turbulence intensity decreases obviously at the medium stage and the preliminary stage of burning because the flow disturbance is eliminated by the mixture of injection flow and main flow

    受噴管潛入影響,結束時刻非常強烈,而間時刻和初始時刻,由於加質與主強迫混合可以消除向下游傳播和擴展,明顯減弱。
  11. Based on the potential theory, linear and fully nonlinear aerodynamic forces and motions of a wing flying above sea - waves are studied numerically. and the effects of the characteristic parameters of wing and sea waves on the aerodynamic forces are acting on the wig are analyzed systematically in this thesis

    本文基於勢理論計算研究了二維和三維機翼在風浪線性和全非線性力及其運響應,全面分析了機翼和波浪特徵參數對影響,得出了很多有意義結果。
  12. All kinds of natural and human factors, including climate, organism, landform, m other rock and material, and human disturbance, influenced the genesis and devel opment of soils in shunde ecological paradise, guangdong province

    廣東省順德生態樂園內土壤形成發育受候、生物、地形地貌、母質母巖和人為干等5大因素影響,其人為活是導致土層結構破壞和水土主要原因。
  13. Abstract : all kinds of natural and human factors, including climate, organism, landform, m other rock and material, and human disturbance, influenced the genesis and devel opment of soils in shunde ecological paradise, guangdong province

    文摘:廣東省順德生態樂園內土壤形成發育受候、生物、地形地貌、母質母巖和人為干等5大因素影響,其人為活是導致土層結構破壞和水土主要原因。
  14. Then the traditional pd controller and gain - scheduling fuzzy pd controller were designed to realize path following of parafoil system. simultaneously, several control strategies were brought forward in view of the basic flight properties of parafoil system. the important one was described as following : the

    同時,基於翼傘系統基本運特性,提出了一系列有針對性控制策略,其重要一條是,將平均風影響在軌跡歸航修正,而大影響作為干由控制器來補償。
  15. The unstructured meshes of the global flowfield are made. 3. the program to solve the six - freedom - of - degree dynamics equation and the kinematics equation of the missile are worked out

    由於非均勻力干作用,其力與外掛物單獨飛行時有較大不同,獲取分離過程力數據是解決這一問題關鍵和難點。
  16. 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:軸穩定性模型,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,在公開文獻有一些二維模型發表.本文提出了一類考慮壓機徑向對失速影響穩定性模型.計算結果表明壓軸向往往隨著徑向產生,徑向強度影響壓穩定性,在葉尖還是葉根首先產生失速與壓機基元葉柵特性密切相關.本文對軸機二維和三維穩定性模型計算結果進行了對比分析
  17. 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

    穩定性模型,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,在公開文獻有一些二維模型發表.本文提出了一類考慮壓機徑向對失速影響穩定性模型.計算結果表明壓軸向往往隨著徑向產生,徑向強度影響壓穩定性,在葉尖還是葉根首先產生失速與壓機基元葉柵特性密切相關.本文對軸機二維和三維穩定性模型計算結果進行了對比分析
  18. Because it is very turbulent inside a cumulonimbus cloud, the water droplets and ice crystals in it will break up and become electrically charged

    由於積雨雲內有急劇,雲水珠和冰粒便會分裂而產生電荷。
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