The Joukowski airfoil problem is the simplest application of conformal mapping to airfoil design.
joukowski問(wèn)題是最簡(jiǎn)單的翼型形映射應(yīng)用到機(jī)翼設(shè)計(jì).
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An effective aerodynamic optimization design method of transonic airfoil is given.
提出了一種有效的跨音速翼型氣動(dòng)優(yōu)化設(shè)計(jì)方法.
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In the design page, submit the form to design the first airfoil.
在設(shè)計(jì)頁(yè), 遞交表格設(shè)計(jì)第一翼型.
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The numerical algorithm is applied for flow over an NACA 0012 airfoil with satisfactory effect.
經(jīng)對(duì)繞NACA0012翼型無(wú)粘流動(dòng)計(jì)算的驗(yàn)證,收效明顯.
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The high speed airfoil type wind turbine has the highest efficiency in high wind speeds.
高速機(jī)翼型風(fēng)輪機(jī)在高風(fēng)速下達(dá)到最高的使用效率.
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Lastly, the paper programs to simulate FRP airfoil FW moulding by VC ++.
最后, 本文用VC++進(jìn)行編程,從而模擬FRP飛機(jī)機(jī)翼FW成型 整個(gè)過(guò)程.
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Airfoil flutter is one of the important problems in aeroelasticity.
在氣動(dòng)彈性力學(xué)中,機(jī)翼振顫是一個(gè)非常典型的問(wèn)題.
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In this regard, several are given based on existing designs, eg, the SD 7037 airfoil and others.
在這方面, 有幾個(gè)版本,基于現(xiàn)有翼型設(shè)計(jì),例如, sd7037翼型等.
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The Web version the code allows for the prescription the inviscid velocity distribution about the airfoil.
網(wǎng)上版的代碼允許處方粘速度分布的翼型.
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The experimental results of NACA 0012 airfoil dynamic pressure measurement are given here.
12翼型動(dòng)態(tài)測(cè)壓的實(shí)驗(yàn)結(jié)果,初步分析了影響翼型動(dòng)態(tài)氣動(dòng)特性的因素.
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The given airfoil is then analyzed to determine, say, its velocity distribution.
由于機(jī)翼的分析,以確定那是說(shuō), 它的速度分布.
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A supporting surface of an airplane ; an airfoil a wing.
飛機(jī)有后掠翼的圓滑的機(jī)翼.
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The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.
對(duì)帶振蕩的快速上仰翼型的非定常分離流問(wèn)題進(jìn)行了計(jì)算研究.
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How does the brake act on the paraglider airfoil?
剎車(chē)是如何作用于滑翔傘的翼型?
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Two pieces of foam are sandwiched onto the center piece and sanded to an airfoil shape.
兩件是泡沫夾心到中心片和磨光的機(jī)翼形狀.
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The properties of bifurcation points of airfoil flutter with cubic nonlinearity in incompressible flow are studied.
對(duì)定常空氣動(dòng)力作用下、含立方非線性剛度的二元機(jī)翼顫振系統(tǒng)的分叉點(diǎn)進(jìn)行了研究.
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A supporting surface of an airplane ; an airfoil or a wing.
飛機(jī)尾部組成部分的垂直機(jī)翼.
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The mathematical transformation is fixed and the airfoil is moved to generate different airfoil geometries.
數(shù)學(xué)變換是固定機(jī)翼的翼型幾何移到產(chǎn)生不同.
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The airfoil shape is then adjusted until the desired velocity distribution is obtained.
然后是調(diào)整翼型的形狀,直到取得預(yù)期的速度分布.
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