wing plate 中文意思是什麼

wing plate 解釋
翼板
  • wing : n 1 翼,翅膀;鳥;鳥群;飛行,飛翔。2 (飛機)機翼;翼狀物;(汽車的)擋泥板;〈詩常 pl 〉船帆。3...
  • plate : n 1 厚金屬板 〈cf sheet〉 板(片);(記有姓名等的金屬)牌子,(尤指醫生的)招牌,藏書牌;【印刷...
  1. The new technique allows first order shear deformation plate theory ( fsdpt ) or classical plate theory ( cpt ) to be used for modeling built - up wing structures, sandwich wing structures or the wing structures which the volume between upper and lower skin is empty or solid with a ' general planform

    根據翼面的幾何和結構特點,新技術能夠自主選擇經典板理論( classicalplatetheory ,簡稱cpt )或第一階剪切變形板理論( firstordersheardeformationplatetheory ,簡稱fsdpt ) ,具有模擬空心、實心、夾層和組合等形式的翼面結構及三維建模的能力。
  2. First, the repeated structural analyses for static and dynamic characteristics are needed in the integrated optimization of composite wing structures. in this situation, the finite element model ( fem ) is time - consuming, while the continuum equivalent plate model ( epm ) is more efficient and often used

    首先,復合材料翼面結構綜合優化設計需要反復進行結構靜力和動力特性分析,如果採用有限元模型( finiteelementmodel ,簡稱fem ) ,則其工作量太大。
  3. The influence of shearing deformation causes the non - uniform stress in the wing plate of the box girder, especially the cantilever box girder

    摘要剪切變形的影響使得箱形梁的翼板中出現應力不均勻現象,尤其是懸臂箱形梁剪力滯現象。
  4. At present, the equivalent plate methodology based on global ritz solution technique has been used in the studies of aeroelasticity and aeroelastic optimization of composite wing structures, but it stiff exits space to develop

    鑒於此,常常採用連續的等效板模型( equivalentplatemodel ,簡稱epm ) 。目前,基於全局ritz求解技術的復合材料翼面結構等效板方法已用於氣動彈性的基本研究和優化設計,但還不夠成熟。
  5. A new equivalent plate modeling technique for composite wing structures is developed in the present work

    因此,本文發展了一種新的復合材料翼面結構等效板建模技術。
  6. We studied four eddy viscosity models ( evm ) and three nonlinear easm models in detail. the two - equation turbulence models are validated through simulating the flow fields over flat plate, airfoils and onera m6 wing. the capabilities of different turbulence models are accessed in this study

    加入兩方程湍流模型后,通過對平板、翼型、 oneram6機翼等繞流流場的數值計算,驗證了加入的各湍流模型的準確性,測試了它們對不同湍流流場的預測能力。
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