偏轉翼 的英文怎麼說

中文拼音 [piānzhuǎnyì]
偏轉翼 英文
wing; pivoting
  • 偏 : Ⅰ形容詞1 （不正; 歪斜） inclined to one side; slanting; leaning 2 （只側重一面） partial; prejudi...
  • 轉 : 轉構詞成分。
  • 翼 : Ⅰ名詞1 （翅膀） the wing of a bird 2 （像翅膀的東西） the wing of an aeroplane etc : 鼻翼 wing of...
  1. Positive aileron deflection produces an anti-clockwise moment about the x axis.

    正的副翼偏轉角產生繞X軸的負方向力矩。
  2. Positive aileron deflection produces an anti - clockwise moment about the x axis

    正的副翼偏轉角產生繞x軸的負方向力矩。
  3. The wake survey cannot be used to measure the drag of stalled airfoil or of airfoils with flaps down.

    尾流測量不能用來測量失連狀態下的冀型或襟翼偏轉后的翼型阻力。
  4. The smart rotor with active trailing edge is a new system for reducing the vibration which can adjust the air load of the blade to actively counteract the main harmonic of the force to the fuselage by controlling the deflection of the trailing edge

    主動后緣附翼控制是一種較新的旋翼減振系統，它通過控制后緣附翼的偏轉，調節槳葉的氣動載荷，實現對機體激振力主要諧波分量的主動抵消。
  5. These hinged flight surfaces could deflect airflow to modify the lift, thereby supplying roll control

    這些以鉸鏈連接的飛行翼面能夠偏轉氣流以調整升力，進而控制滾轉。
  6. < uk > the configuration has two tractor propellers, full - span double slotted flaps deflected 45, and a high tail. < / uk >

    < uk >實驗模型有二兩拉力螺旋槳，全翼展雙縫襟翼偏轉45 ，並有高置的水平尾翼。 < / uk >
  7. The configuration has two tractor propellers, full-span double slotted flaps deflected 45°, and a high tail.

    實驗模型有二兩拉力螺旋槳，全翼展雙縫襟翼偏轉45，並有高置的水平尾翼。
  8. Multi - gap - fowler - flap, while deflecting its rudders, simultaneously extends backwards by relatively large scope, which broaden the overall wing - camber and area, so that more additional lift could be attained through improving air - flow boundary layer

    多縫富勒襟翼在襟翼舵面偏轉的同時發生較大幅度的後退，增加機翼整體彎度和機翼面積，通過縫隙氣流改善附面層狀況，因而得到加大的升力增量。
  9. Angle of flap deflection

    襟翼偏轉角
  10. Numerical results show that the present method is effective one for solving the flow around wing with flap deflection

    數值算例表明本方法是求解帶襟翼偏轉的機翼繞流的有效方法。
  11. N - s method for solving the flow around a wing with deflection of flap is presented

    給出了帶襟翼偏轉的三維機翼繞流的一種求解n - s方程的計算方法。
  12. A n - s method for solving the flow around a wing with deflection of flap is presented

    給出了帶襟翼偏轉的三維機翼繞流的一種求解n - s方程的計算方法。
  13. Attaching mesh generation sources to the moving boundary allows a reasonable mesh distribution after remeshing. quadtree data structure is used to accelerate the searching operation during interpolation. results of mesh deforming about a rotating airfoil show that the new spring analogy greatly improves the deforming ability and mesh quality without lowering the efficiency

    以偏轉翼型動網格為例驗證了網格變形技術，結果表明：改進后的彈簧近似方法在保持原有高效率的同時，大大提高了網格變形能力和變形后網格質量。
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