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- The aerodynamic drag of different models at zero angle of attack in the experiment is calculated using the simplified procedure. 在零攻角實(shí)驗時(shí)不同模型的空氣動(dòng)力阻力是采用簡(jiǎn)化方法來(lái)計算的;
- The thickness ratio appeared to have little effect on lift coefficient at zero angle of attack, since the angle of zero lift was largely determined by the airfoil camber. 在迎角為零時(shí),由于零升力主要由機翼中弧線(xiàn)決定,相對厚度對升力幾乎沒(méi)有影響。
- Ffowcs-Williams and Hall were the first to solve the problem of noise radiated from the turbulent flow past a semi-infinite plate of zero thickness at zero angle of attack using this analogy. Ffowcs Williams和Hall是第一個(gè)研究湍流流過(guò)零厚度,零攻角半無(wú)限長(cháng)平板的噪聲輻射問(wèn)題的科學(xué)家。 他們仍然是以L(fǎng)ightill聲類(lèi)比方法為理論基礎,得出了遠場(chǎng)噪聲強度與湍流特征速度是五次方的關(guān)系。
- Mechanism of Transition in a Hypersonic Sharp Cone Boundary Layer With Zero Angle of Attack 高超音速零攻角尖錐邊界層轉捩的機理
- Numerical Simulation of Flow Field for Wraparound Fins Projectile at Zero Angle of Attack 卷弧翼彈零攻角流場(chǎng)數值模擬
- Stability Analysis and Transition Prediction of Hypersonic Boundary Layer Over a Blunt Cone With Small Nose Bluntness at Zero Angle of Attack 零攻角小鈍頭鈍錐高超音速繞流邊界層的穩定性分析和轉捩預報
- AF 2 ITERATION AND ITS PARALLEL ALGORITHM FOR TRANSONIC FLOW WITH LARGE DISTURBANCES IN FREESTREAM-DIRECTION AROUND AXISYMMETRIC BODIES AT ZERO ANGLE OF ATTACK 旋成體零攻角縱向大擾動(dòng)勢流的AF-2迭代及其并行算法
- Angle of attack typically ranges from 3o to 12o for a paraglider. 典型的飛行傘攻角范圍由3度到12度之間。
- The existence of angle of attack reduces the inlet performance. 攻角的存在也在一定程度上降低了進(jìn)氣道性能。
- Jigs for ailerons and tail angles of attack. 用以保證副翼及尾翼安裝角的夾具。
- zero angle of attack 零攻角
- Numerical solutions agree with supersonic linearized potential flow theory as a special case when the mean angle of attack tends to zero and with piston theory in hypersonic case. 作為平均迎角趨于零的特殊情況,本文的數值結果與超聲速線(xiàn)化的位流理論是一致的,在高超聲速情況與活塞理論一致。
- The SHM (single hole microblowing) as a new perturbation active control technique has been applied to the slender body with different model noses at zero sideslip and high angle of attack. 摘要在亞臨界流動(dòng)范圍內,對具有不同頭部形狀的尖拱形細長(cháng)旋成體在無(wú)側滑大迎角下進(jìn)行單孔位微吹氣擾動(dòng)控制實(shí)驗。
- As seen above, the design angle of attack for the second segment is 10 deg. 如上所述;設計攻角的第二部分是10甘醇.
- As seen above, the design angle of attack for the second segment is10 deg. 如上所述;設計攻角的第二部分是10甘醇.
- The commander chalked out his plan of attack. 司令官對進(jìn)攻計劃作了粗略的介紹。
- She hit her knee against the angle of the bed. 她的膝蓋撞到床角上了。
- The conventional tail must be at a negative angle of attack, and the Canard tail at a positive angle. 通常的尾翼必須處于負迎角,而鴨式尾翼則為正迎角。
- It indicated a mismatch in the lower-level comparison in the air data system, specifically with angle of attack. 這表明在大氣數據系統在比較基準方面有匹配不當的問(wèn)題,特別是在迎角狀態(tài)下。
- His fleet emerged from superluminal at just the correct angle of attack, in good formation and proper deployment. 他的艦隊從超光速狀態(tài)出現到這個(gè)位置,攻擊角度恰好正確,隊形完好,部署適當。