straight wing 中文意思是什麼

straight wing 解釋
直翼
  • straight : adj 1 直,一直線的 (opp crooked bent curved )。2 直挺的,向(目標)直進的。3 直接的,連續的。4 ...
  • 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...
  1. Press reports and photographs from the straight - line test at a private airfield in menorca on wednesday indicate that mclaren ' s chrome - liveried car has indeed been slightly tweaked ; with detailed changes mainly to the rear wing, sidepod chimneys and barge boards

    一些媒體和攝象記者認為麥克拉倫的銀色塗裝有些折皺,另外尾翼,側箱的進風口的細節上都有些改變
  2. Abstract : the effects of airfoil geometric parameters on wing " s spacial and polarized scattering characteristics have been systematically revealed. the results of the study indicated that the calculating value of diffraction from trailing edge by using the formula of the straight wedge is very far from experimental results for vertical polarization, and the contribution of thickness of the trailing edge to scattering must be considered in the calculation. the scattering peak of leading edge depends only on radius of airfoil for horizontal polarization. but for vertical polarization, it depends on maximum thickness and the location of maximum thickness. engineering formulas for evaluating all scattering peaks were given in the paper. it is important for the design of low - rcs wing

    文摘:系統地揭示了翼形幾何參數對機翼的空間散射特性、極化散射特性的影響規律.研究發現,在垂直極化狀態下用理論尖劈公式計算機翼后緣繞射的計算結果與實驗結果相差甚遠.提出在垂直極化狀態下機翼后緣繞射的計算必須將后緣厚度考慮在內的見解.對於水平極化,前緣散射波峰只與前緣半徑有關;而對於垂直極化,前緣散射波峰與翼形最大厚度以及最大厚度位置有關.給出前後緣散射波峰的工程估算公式,為低雷達散射截面( rcs )機翼設計提供依據
  3. Go straight into wing on street from the ferry pier and you will find tin hau temple

    從碼頭直入永安街,便可見到天後廟。
  4. Optimal layout about wing amp; amp; fuselage on bi - fuselage aircraft with high aspect ratio straight wing

    大展弦比聯接翼結構重量估算
  5. Structural stiffness effect of single amp; amp; bi - fuselage uav with higher aspect ratio and straight wing

    大展弦比直機翼雙機身飛機中機身與機翼的最佳布置問題
  6. The results calculated with b - l and j - k turbulent models are compared with experimental data. with the examples of some straight wing and sweep wing, the static aeroelastic characterictics of the wing are studied

    分別以某平直機翼和后掠機翼為算例,對機翼的靜氣動彈性問題進行研究,部分計算結果和有關文獻的結果進行了比較,吻合很好,驗證了本文方法及程序的正確性。
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