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1·How does the brake act on the paraglider airfoil?

刹车是如何作用于滑翔伞的机翼的？

2·An airfoil member comprising.

翼型会员包括。

3·Airfoil design technology and criterion are investigated.

进行了叶型设计技术和准则的研究。

4·The airfoil member according to claim 1, further comprising.

翼型会员根据权利要求1，进一步包括。

5·In the design page, submit the form to design the first airfoil.

在设计页，递交表格设计第一翼型。

6·In the method, such an airfoil is termed a four-segment airfoil.

在方法，这种称为翼型四个部分机翼。

7·An airfoil adapted to be supported on an aircraft fuselage comprising.

翼型适应予以支持对飞机机身组成。

8·An airfoil as recited in claim 17, wherein said airfoil means includes.

翼型作为背诵，在索赔17，其中，表示翼型的手段包括。

9·Optical lift is different from the aerodynamic lift created by an airfoil.

光学提拉力与机翼翼面产生的空气动力不同。

10·The given airfoil is then analyzed to determine, say, its velocity distribution.

由于机翼的分析，以确定那是说，它的速度分布。

翼型

1·The flaperons have their own airfoil, and are hung below the wing trailing edge to supply them with fresh undisturbed air for maximum control effectiveness even at low speeds.

襟副翼有自己的翼型，并挂在机翼后缘下方新鲜空气原状的速度控制在较低的最大效益，甚至他们与供应。

2·So for Mid reflection airfoil, the wing could fly normally with only A and B anchor.

所以对于中反射翼型来说，只要A，B 两组绳就能正常飞行。

3·To put the method in some perspective, it helpful to briefly outline the two general approaches to airfoil design.

把一些观点方法，它有助于扼要介绍两个一般方式翼型设计。

4·In the design page, submit the form to design the first airfoil.

在设计页，递交表格设计第一翼型。

5·As airfoil thickness is increased, the average pressure drag, affected by leading edge vortex is reduced even to be negative, and meanwhile friction has little increase.

由于前缘涡的影响，翼型厚度增加，平均压差阻力系数变小，甚至会出现负值。

机翼

1·How does the brake act on the paraglider airfoil?

刹车是如何作用于滑翔伞的机翼的？

2·Direct methods are based on the design-by-analysis approach in which the airfoil shape is specified first.

直接的方法是基于设计逐案分析的方法是机翼形状指定第一。

3·The sloping metal ceiling panels free of penetration s read as a sweeping airfoil structure that floats above the space, drawing passengers along its arcing central spine.

屋顶倾斜的金属面板凸显在外，犹如漂浮在空间之上的巨型机翼，将乘客引入到其中心弧形脊椎中。

4·Thus, it would be more advantageous to specify the velocity distribution from the outset and from that determine the airfoil shape.

因此，它会更有利，指明速度分布，从一开始就确定，从机翼形状。

5·In the method, such an airfoil is termed a four-segment airfoil.

在方法，这种称为翼型四个部分机翼。