非湍流的 的英文怎麼說

中文拼音 [fēiliúde]
非湍流的 英文
non-turbulent
  • : Ⅰ名詞1 (錯誤) mistake; wrong; errors 2 (指非洲) short for africa 3 (姓氏) a surname Ⅱ動詞1 ...
  • : [書面語]Ⅰ形容詞(湍急) rapid; rushing; torrential; swiftⅡ名詞(急流的水) rapids; rushing waters
  • : 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
  • 湍流 : 1 (急流) swift current; rushing waters; torrent; rapids 2 [物理學] turbulent flow; turbulence; ...
  1. In section one, by using fice scheme and time - gcm, a model of trace gases and oh airglow affected by gravity wave is set up, then the propagation of nonlinear gravity wave and the effect on trace gases and oh airglow are analyzed. the result shows gravity wave excited by tropospause forcing can propagate stably to the mesosphere through the stratosphere so that energy and momentum can be transferred from one region to another. in this process, gravity wave undergoes growth, overturning, convection and breaking

    在第一部分工作中,利用全隱歐拉格式和全球熱層-電離層-中間層-電動力學環耦合模式( time - gcm ) ,對重力波線性傳播及其在傳播過程中對中高層大氣中氧族和氫族成分和與之密切相關oh氣輝輻射影響進行了數值模擬,結果表明,從對層向上傳播重力波經歷了產生、發展、飽和、對產生直至破碎線性演化,大氣等溫結構加速了重力波在中層頂區破碎,重力波線性傳播是小尺度對產生一個重要源。
  2. The non - local turbulence parameterization, i. e., transilient theory was used in the host model mm4 to simulate the turbulent activities of the atmosphere

    在中尺度區域模式mm4基礎上對其中參數化方法作了改進,嘗試用局地閉合方法代替局地
  3. It adopts reynolds time - average n - s equation and k - ? turbulence model to calculate the inner 3 - d viscid turbulence flow of centrifugal pump. in the unstructured grid, the governing equations are discretized with finite volume method based on finite element method. then the pressure correction method is used to carry out numerical calculation

    而後採用基於雷諾時均n - s方程與標準-模型來求解離心泵葉輪內三維粘性紊,在結構化網格中,採用基於有限元有限體積法對方程進行離散,用壓力校正法進行數值求解。
  4. The effects of air ' s absorption of heat, scatter, turbulent and thermal blooming on the laser beam transmitting under the air breakdown threshold value are analysed when laser transmit in the air and the result can be used designing of the laser system

    摘要系統分析了激光在大氣中傳輸時在擊穿閾值以內,由於大氣汽溶膠吸收、散射、大氣、大氣熱暈等線性線性問題對光束控制系統影響,為激光系統提供指導。
  5. The instability in the natural convection boundary layer initiates with the buoyancy eigenmode and develops into non - linear stage with the turbulization of the buoyancy eigenmode. in the mean time, the invisid eigenmode at the inflexion point appears and begins to increase at the outer layer. experimental results show that the turbulent layer near the maximum velocity point can be detected while the reformed grashof number

    自然對邊界層穩定性由浮力振型失穩開始,並隨著浮力振型化進入線性階段,與此同時,無粘性振型在外層開始失穩。實驗結果表明,修正格拉斯霍夫數grashof
  6. Turbulent fluxes over heterogeneous surfaces and the blending height

    均勻地表通量和摻混高度
  7. In chapter 3, the subgrid eddy - viscosity model for large eddy simulation is applied to calculate the three dimensions unsteady periodic turbulent flow in yantan francis turbine. the pulsating characteristics of some main physical parameters in flow field are found. the calculated axial water thrust of hydraulic turbine agrees with the model - test value

    第三章採用大渦模擬亞格子渦粘模型,對巖灘混式水輪機場進行三維定常分析,得到了場中各物理量脈動特性,計算出ms軸向水推力與模型試驗值大小相當;同時論證了對于下機架承重式水輪發電機組可採用其推力軸承負荷作為水電站廠房振動最大垂直激振荷載。
  8. We must keep up - stream. you see, sir, he went on, if once we dropped to leeward of the landing - place, it s hard to say where we should get ashore besides the chance of being boarded by the gigs ; whereas, the way we go the current must slacken, and then we can dodge back along the shore

    「你看,先生,我們必須逆水行舟, 」他接著說道, 「要是一旦我們錯過了那個著陸地點,很難說我們會在哪兒上岸,除是在那兩只劃子邊上停船,反之,照我們現在這個航向走,勢必是要減弱,然後我們就可以沿著海岸退回來。 」
  9. Due to its complexity of the problem, the theories and experiment results obtained are discrepant, and some of them are even contrary one another. started from the influence by movement rules of small cavities and solid particles, the mechanisms of combined effect of cavitation and sand abrasion are study in this thesis from the aspect of the turbulent coherent structure near the wall. first, a dynamic equation is established for a single spherical bubble and single spherical sand under the non - turbulent coherent structure near the wall, and then a dynamic equation established under the turbulent coherent structure near the wall

    首先從理論上推導出在典型邊界層模式擬序結構下空泡與固體顆粒近壁區運動方程,然後推導出近壁擬序結構作用下空泡與固體顆粒近壁區運動方程,再將兩種不同條件下運動方程進行比較,指出近壁區擬序結構對空蝕與磨損發生具有決定性意義,即正是由於擬序猝發作用存在,才使得空泡、沙粒對壁面空蝕與磨損作用得以發生。
  10. Based on the vibration test in yantan hydropower house, in this paper the author adopt les method which belong to three dimensions unsteady turbulent flow numerical analysis to simulate vibration resource characteristics of hydrogenerator set, a harmonic vibration model of powerhouse substructure is put forward to carry out firstly a precise modal analysis and dynamic response analysis for generator floor. the numerical calculation results agree well with the surveyed data in situ

    本文結合巖灘水電站廠房振動試驗研究,採用定常數值分析大渦模擬方法進行混機組水力振動振源模擬;提出一種水電站廠房下部結構簡諧振動模型,首次進行了發電機層樓板結構精確模態分析和水力激振荷載下動力響應分析,各項計算結果與實測數據吻合良好。
  11. Only 6 % of congolese have access to electricity and more power will be needed to get at the country ' s trove of minerals

    從理論上講,在剛果河水沿路建造多個水壩宏偉計劃將提供三萬九千兆瓦特能量,這些足夠為整個洲大陸提供能量。
  12. Abstract : approximate methods for calculating aerodynamic heating rates on space shuttles are discussed. various methods are given for predicting the heating rate at axisymmetric stagnation points, general three dimensional stagnationpoints and the leading edge stagnation point of wings. numerous laminar and turbulent heating techniques for flat plates and cones are analyzed and compared. a brief review of some methods is presented to predict heating rate for winward centerline and lateral direction off the symmetry plane. the results show that the methods are simpler and can guarantee enought precision for predicting aerodynamic heating environment of space shuttles

    文摘:介紹了國內外預測航天飛機氣動加熱工程計算方法.給出了軸對稱、軸對稱和機翼前緣等各種外形駐點熱密度計算,分析和比較了平板、錐體密度計算各種方法,概述了航天飛機迎風面中心線和離開中心線橫向熱密度計算.計算結果表明,本文方法用在航天飛機氣動熱環境初步設計中比較簡單並且有足夠精度
  13. Secondly, we numerically simulate the turbulence behavior of one - dimension fpu model and obtain probability density functions of the velocity differences in different conditions. we use tsallis statistics to fit the probability density functions and find out it was fitted very well

    其次,我們對一維fpu模型中類似行為進行了數值模擬,得到不同條件下速度差概率密度函數,並利用tsallis統計對其進行擬合,發現兩者符合得常好。
  14. The additional sub - scale flux is mainly determined by the average grid value, coefficient of variation and correlations among the meteorology parameters. ( 2 ) the additional sub - scale turbulence flux is composed by two parts, one part is induced by the correlations among the transfer coefficient, surface temperature and soil humidity, another is caused by non - line relationship between the transfer coefficient and roughness, stability

    ( 2 )均勻分佈引起附加次網格地表通量主要由兩部分組成:一是地表次網格上輸送系數和地表溫度、濕度相關項,另一是由於模式中計算整體輸送系數時,整體輸送系數是地表粗糙度和穩定度線性函數所造成擾動項。
  15. Based on prandtl ' s momentum transportation, this paper calculates in detail the physical quantities such as eddy viscosities, and ratio of eddy viscosity to motion viscosity, total stresses with respect to relative position in three regions of viscous sub - layer, buffer layer, and main turbulent stream for non - newtonian fluid flowing turbulently in ducts, which according to karman ' s three layer models and measurement of fluid parameters in evaluation apparatus, discusses the influence of polymer drag reduction on flowing properties of non - newton fluid, analyzes quantitatively principle of turbulent reduction phenomenon and condition of increasing reduction rate

    摘要以普蘭德動量傳遞理論為基礎,按照卡門三層模型,通過室內模擬環道用0號柴油及加入減阻劑在圓管內動參數測定,計算了牛頓型體管內邊界層內層、過渡層、中心粘度,渦粘度與運動粘度比、總應力隨相對位置變化等定量參數,探討了高分子減阻劑對牛頓動特性影響,對減阻現象機理與增大減阻率條件進行了定量分析。
  16. Flow details of measurement indicate that the coupling of periodic separated flow ( such as low frequency swinging of separation line ) with nozzle flow may cause aft - end internal flow unsteady. recirculation flow gains more energy from the main flow, at the same time the turbulence intensity increases

    通過對測量結果分析,我們認為分離周期性(如分離線低頻擺動)與噴管動相耦合,會造成燃燒室尾部穩態效應增強,增加了迴區從主中獲得能量,也加劇了脈動。
  17. 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,結束時刻脈動常強烈,而中間時刻和初始時刻,由於加質與主強迫混合可以消除氣擾動向下游傳播和擴展,脈動明顯減弱。
  18. Nonlinear turbulence models in shock boundary - layer interaction

    邊界層相互作用線性模式
  19. First, in the field of atmospheric dynamics the developments in dynamics of diabatic waves and low - frequency waves, the dispersive effects of turbulence and nonlinear atmospheric waves are re - viewed

    在大氣動力學領域,主要介紹了絕熱波和大氣低頻動力學、頻散效應和大氣線性波動等方向研究進展。
  20. Abstract : some typical results of computation on the shock ( blast ) wave interaction ( 2 - d and 3 - d ) with bodies and its experimental validation in shock tube are summarized, the suggestion for improving the numerical method ( difference scheme and grid systems ), developing 3 - d optical quantitative visualization technology and further studying the unsteady turbulent flow are put forward

    文摘:給出了在二維和三維條件下激波(爆炸波)與物體相互作用一些典型計算結果,概括總結了激波管中實驗有效性,提出了改進數值方法(包括差分格式,網格系統) ,發展三維光學定量可視化技術和進一步研究定常建議。
分享友人