非定常解析 的英文怎麼說

中文拼音 [fēidìngchángjiě]
非定常解析 英文
time dependent analysis
  • : 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 ...
  • : 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...
  • : 解動詞(解送) send under guard
  • : Ⅰ動詞1. (分開; 散開) divide; separate 2. (分析) analyse; dissect; resolve Ⅱ名詞(姓氏) a surname
  • 解析 : analysis; resolution; analyzing; resolving解析幾何 [數學] analytic geometry; cartesian geometry; ...
  1. The fundamental ideas and methods of this paper are also illuminated in this chapter. in chapter two, a one - dimensional and semi - closed shallow sea mode is studied. the approximate analytical expressions of the water level at the top of the bay induced by the nonlinear interaction between the storm surges and the astronomical tides are obtained by using the perturbation method

    在第二章里,研究了一維半封閉水域中的風暴潮與天文潮線性相互作用的問題,用攝動方法求出了具有實際意義的海灣頂部增水水位的一階近似表達式,並給出了增水過程曲線。
  2. A simply and analytical formula of the axial light intensity distribution behind a circular aperture is derived by using the helmhotz - kirchhoff integral theorem and the kirchhoff ' s boundary conditions. it is studied the nonparaxial on - axis intensity distribution throughout the whole space behind a circular aperture. an accurate formula to calculate the fresnel number of circular aperture is presented and the validity of usual fresnel number formula is reexamined. by using the analytical formula and diffraction integral formula, some numerical simulation comparisons are done, and it is shown that the results of the two methods are completely coincident

    用亥姆霍茲-基爾霍夫積分理和基爾霍夫邊界條件,推導出了平面波經小圓孔傍軸衍射時軸上強度的簡單表達式,研究了平面波經小圓孔后整個衍射空間傍軸的軸上光強分佈.給出了計算圓孔菲涅爾數的精確公式,重新檢查了通的菲涅爾數公式的有效性.數值計算顯示,應用表達式所得的結果與應用衍射積分公式所得的結果完全一致
  3. According to non - newtonian fluid mechanics theory and mathematical method, conbined with plunger moving property, the hypothesize fluid is imcompressive, hydraulic radius of flow of liquid in crevice is very little, and it is laminar flow, the flow is treated fixed continuous flow at every instant position of plunger, equation of motion and boundary condition were set up in condition of concentric and eccentric of pump barrel and plunger

    運用牛頓流體力學理論和數理方法,結合抽油泵柱塞運動特點,假設液體為不可壓縮的,液體在縫隙中流動的水力半徑很小,呈層流流動,柱塞在每一位置的瞬間,流動做流處理,建立了泵筒與柱塞同心和偏心兩種情況下運動方程和邊界條件,引入無量綱坐標、無量綱速度和柱塞與泵筒偏心配合時的縫隙高度,並給出縫隙流流速、流量的
  4. When the element studied lost the stability during the elastic - plastic period, the stability balance equation turn to the special coefficient differential equation, and the analytic value cannot be got

    當所研究構件是在彈塑性階段失穩時,穩平衡微分方程變成系數微分方程,而無法求得其
  5. Improved tanh - function method and the new exact solutions for the general variable coefficient kdv equation and mkdv equation

    可壓等熵流線性方程顯式的推導
  6. Associated with a project of the planned xuefengshan tunnel with 7. 6 km long during the construction of shaoyang to huaihua expressway in hunan province of shanghai to ruili national trunk highway, this paper firstly makes an introduction of the frequently - used analysis & computation methods for tunnel supporting structure. then, based on the analysis of the basic theory about the interaction mechanism of surrounding rock and support structure, a spatial computation model is made, a coupling numerical computation method with 3 - d elastic - plastic finite element and infinite element is proposed, and a comprehensive analysis has been made to the effects of the overall stability and safety of the surrounding rocks of different characteristics, different classes and under different construction methods. and thus the problem of 3 - d infinite region to which applying the general finite ca n ' t do has been resolved

    6公里的雪峰山隧道工程,首先介紹了隧道支護結構的用分計算方法;然後通過對隧道施工過程中,洞室穩性與支護結構相互作用機理的深入分,建立了隧道施工過程的空間計算模型,提出了採用三維彈塑性有限元-無限元耦合的數值計算方法,綜合分了隧道在不同圍巖特性和圍巖類別條件下,以及不同施工開挖方案等對隧道圍巖整體穩和安全性的影響,從而決了通用有限元方法難以決的隧道三維無限域問題;其可充分發揮有限元法在分線性方面的有效性和成熟性,以及無限元法在分處理無限域和半無限域方面的精確性和簡便性,為隧道施工過程中圍巖的穩性分開辟了一條新的途徑。
  7. The transient mathematical equations are addressed for the coupled heat and moisture transfer by taking account of moisture accumulation procedure. an analytical method by means of the transfer function is proposed to predict the transient distributions of temperature and moisture content at different interfaces in walls. a numerical analysis approach based on an efficient finite - difference method is developed to deal with the procedure of coupled heat and moisture transfer in a multilayer wall with nonlinear boundary conditions considered

    建立了考慮濕積累過程的瞬態熱濕耦合模型,在方程中引入了濕積累項;發展了一種傳遞函數方法進行墻體內不同剖面處溫度和含濕量的動態預測;首次提出了一種基於有效有限差分法預測線性邊界條件下多層多孔結構內的傳熱傳濕過程的數值分方法,求過程中考慮了瞬態邊界條件,從而避免了通處理中由於邊界條件設數而給計算帶來的誤差,對于多層結構每一層物性參數的連續性,則採用了有效的有限差分逼近處理。
  8. Our numerical investigation in the original electronic relaxation oscillator shows very good agreement with the analytical conclusions

    對實際的電張弛振子模型的數值調研結果與此結論好地性符合。
  9. Then the steady and unsteady subsonic, transonic and supersonic viscous flows around airfoil and some aircraft are numerically simulated. the 3 - dimensional unsteady navier - stokes equations are solved using the implicit lu - nnd algorithm, with baldwin - lomax turbulent model. on the basis of simulating unsteady viscous flow, coupling the structure dynamics equations, the problems of static aeroelasticity and flutter are investigated for wings and elevator

    在模擬粘性繞流的基礎上,與顫振運動方程相耦合,分別對機翼和全機流固耦合現象中顫振問題進行了研究,準確求跨音速顫振臨界速度,分機翼和全機的從亞音速到超音速范圍的顫振規律,並研究分了機翼飛行迎角變化對顫振速度的影響。
  10. In modern aircraft design, there is an urgent requirement for accurate, efficient and easy - to - use numerical analysis tools. for this purpose, this thesis introduces recent progress in the generation and application of cartesian grid with tree data structure and adaptive refinement. coupled with hybrid grid techniques, euler and navier - stokes equations are solved

    本文針對現代飛行器設計中對實用、高效、準確的氣動力分工具的迫切需求,基於叉樹數據結構,發展了一種自適應直角切割網格方法,採用混合網格技術,實現了對流場euler和navier - stokes方程的計算求,進一步完成了復雜增升裝置繞流和外掛物分離投放流場的數值模擬。
  11. The paper researches the transient time precision and the following problem of the results developing with time for 2 - d high order blocking and matched method, at the same time, anlysing the stability of high order methods including boundary conditions. the results show that the domain decomposition and matched method using high order method can follow the time developing solution of taylor problem well, the computation result of the flow over a single or two tandem arranging circular cylinder agree the experiment and others " results well, moreover, the panting results of lift and drag coefficient are better than others

    本文利用高精度分塊耦合求方法,對其瞬態時間精度和時間發展的跟隨性問題進行了研究,同時也對包含邊界條件的線法高精度格式的穩性也作了分,研究結果表明高精度的分塊耦合求方法可以很好地跟隨taylor問題的時間發展,與單圓柱繞流和雙圓柱繞流的實驗結果比較以及他人結果比較符合很好,對升阻力系數在渦脫落時的脈動問題的結果優於他人結果。
  12. Second, the structural dynamic equations for blades are introduced in this paper. through numerically solving the aerodynamics - structure coupled equations, a 2 - d unsteady viscous flow in a single cascade is investigated under flow - structure coupled conditions, and a preliminary analysis of the cascade flutter is prosecuted

    其次,本文引入葉片結構動力學方程,通過數值求氣動結構耦合方程體系,研究了氣固耦合條件下葉柵內的二維粘性流動,並初步進行了葉柵的顫振分
  13. Abstract : based on the analysis of the pressure equation of filling flow in injection molding, finite - element method is employed to solve the transient pressure field with moving free form boundary

    文摘:在分注塑充填流動壓力方程的基礎上,採用有限元方法求充填過程中、具有移動邊界的壓力場。
  14. The investigation in this dissertation shows the capabilities of ausm + scheme, such as the exact resolution of shock, low numerical dissipation, simple and requiring less computational effort. the successful applications on supercritical airfoils and wings show that the present flow solvers based on ausm + scheme are of valuable and promising in practical application

    通過本文的研究工作,展示了ausm +格式的激波高度、數值耗散小、編程簡潔、計算量較小等特性,同時,將其成功地應用於跨音速超臨界翼型、機翼的氣動特性的數值模擬和顫振研究中,具有一的工程應用價值和良好的發展前景。
  15. A study of unsteady flow of viscoelastic fluid by ananlyticl method

    周期壓力梯度下粘彈流體流動的法研究
  16. In this thesis, finite volume method and dual - time stepping method are employed to solve the 3 - d unsteady euler equations. the unsteady flow field around a finite - span flapping wing is simulated. the lift and thrust of the flapping wing for different cases are calculated

    本文運用有限體積法結合雙時間推進技術求三維歐拉方程,模擬了有限翼展機翼在同時具有上下拍動和俯仰運動狀態下的流場,計算了不同狀態下撲翼的升力及推力,分了各個影響因素對撲翼氣動特性的影響。
  17. Upon the concentration distribution of the ammonia water mixture in liquid bulk during absorption, two analysis methods were established. one is based on optical fundamental theory of the interference fringes phenomenon. the other is based on the calculation of mass transfer equation

    一種方法是利用光學基本原理,通過對干涉圖像的得到液體內部濃度分佈;另一種方法是通過對邊界條件下的質擴散方程求,得到液體內部濃度分佈。
  18. A useful technique has been provided and developed for the researching and analyzing the factors and variation of flow field in the intake duct of diesel engine. to find out a new method to measure flow measurement, different intake duct on different conditions are experimented and researched by real - time holographic interferometry. real - time holography interferometry has many characteristics, such as high precision, non - destructive, high contrast of interference fringes and full field test

    該方法具有精度高、接觸、條紋對比度好、對被測物體形狀和表面無特殊要求的特點,實驗了對三維流動過程的可視化實時採集,為了和分不同流量、不同結構參數下進氣道內氣流運動狀態和流動特性的變化關系及其影響因素提供了一種有效的測試手段。
  19. A high accuracy, high resolution numerical method ( lu - sgs - ge scheme and 4th order muscl tvd scheme ) is applied to calculate the unsteady flow field

    在計算網格移動下的流場時採用了高精度、高度的數值計算方法? ? lu - sgs - ge隱式格式和高階muscltvd格式。
  20. Secondly, we investigate the nonlinear dynamics if the system by using the multiple method of scale, and discuss the stability of the steady - state solution

    其次對系統進行了線性動力學的分,利用多尺度方法獲得了一次近似響應,討論了的穩性。
分享友人