報文結尾 的英文怎麼說

中文拼音 [bàowénjiēwěi]
報文結尾 英文
end of message eom
  • : Ⅰ動詞1 (告知; 報告) report; declare; announce 2 (回答) reply; respond; reciprocate 3 (答謝)...
  • : Ⅰ名詞1 (字) character; script; writing 2 (文字) language 3 (文章) literary composition; wri...
  • : 結動詞(長出果實或種子) bear (fruit); form (seed)
  • 結尾 : 1. (末尾; 結束的階段) ending; winding-up stage; finis; terminal 2. [音樂] coda3. [計算機] trailing end
  1. The surface panel method has been applied to predict the hydrodynamic performance of highly skewed propeller. the surface of propeller and its trailing vortex are discreted by a number of small hyperboloidal quadrilateral panels with constant source and doublet distribution. for highly skewed propeller, the conventional method generating grid oriented along constant radii will result in a high aspect ratio and a high skewness and a twist panel near the propeller tip on blade surface, which result easily in incorrect calculation results of velovity on blade surface, even in iteration divergence and calculation failure. a “ non - conventional grid ” is developed to acoid these problems. this grid can effectively solve the problem of the calculation and convergence for highly skewed propeller. the non - linear kutta condition of equal pressure on upper and lower at the trailing edge is executed by the iterative procedure. by sample calculating, the obtained results are satisfied the experimental data

    採用面元法預大側斜螺旋槳水動力性能,螺旋槳表面及渦面離散為四邊形雙曲面元,每個面元上布置等強度源匯和偶極子分佈.對于大側斜螺旋槳而言,槳葉表面採用常規的等半徑網格劃分方法在近葉梢處將導致大展弦比、大側斜和扭曲面元,這容易使槳葉表面速度的計算果不正確,甚至會導致迭代過程發散及計算失敗.中建立了一種「非常規網格」劃分方法,能有效地解決大側斜螺旋槳的計算和收斂問題.槳葉隨邊處通過迭代實現非線性等壓庫塔條件
  2. Lastly, previous vane are analysed by fluent, we calculate the pressure distribution chart and report chart of each wing form, then alter the torsion angle and the airfoil form of the vane respectively, finally ascertain the influence curve of the torsion angle and the airfoil form of the vane on which act the lift power

    最後,通過fluent對設計出的葉片分析,得出其壓力分布圖和告圖。然後從改變葉片的扭轉角度和翼型兩個方面分析其對升力和阻力的影響。得出葉片的扭轉角和翼型對升阻比的影響曲線,在章的部分估算了無人機的一些性能參數。
  3. 4 yarnell w s, roberts j w. mechanism of intrinsic transcription termination and antitermination. science, 1999, 284 : 611 - 615. 5 gusarov i, nudler e. the mechanism of intrinsic transcription termination

    本論道了一種不依賴終止子預測的新方法- rnall法,它建立於我們最近開發的rna局部二級構和以前發表的兩種u -部分數計算方法。
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