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Combined droop nose and trailing-edges morphing effects on airfoils aerodynamics

机译：组合下垂鼻子和尾翼的边缘对翼型空气动力学的影响

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M. A. Aziz; M. Mansour; D. Iskander; A. Hany;
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年度 2019
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1. Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose [J] . De Gaspari Alessandro, Moens Frederic International journal of aerospace engineering . 2019,第PTa2期

机译：具有变形下垂鼻子的支线飞机的先进高空装置的空气动力学形状设计和验证
2. Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose [J] . De Gaspari Alessandro, Moens Frederic International journal of aerospace engineering . 2019,第PTa2期

机译：用于变形下垂鼻子的区域飞机先进高升机装置的空气动力学设计与验证
3. Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose [J] . Alessandro De Gaspari, Frédéric Moens International journal of aerospace engineering . 2019,第4期

机译：用于变形下垂鼻子的区域飞机先进高升机装置的空气动力学设计与验证
4. Experimental and Numerical Investigation of Aerodynamic Performance of Airfoils Fitted with Morphing Trailing-edges [C] . Hasan Kamliya Jawahar, Qing Ai, Mahdi Azarpeyvand AIAA/CEAS aeroacoustics conference . 2017

机译：尾翼变形翼型气动性能的实验和数值研究
5. Estimation of morphing airfoil shapes and aerodynamic loads using artificial hair sensors. [D] . Butler, Nathan Scott. 2015

机译：使用人工毛发传感器估算变型的机翼形状和空气动力负荷。
6. Flow visualization over a thick blunt trailing-edge airfoil with base cavity at low Reynolds numbers using PIV technique [O] . Gholamhossein Taherian, Mahdi Nili-Ahmadabadi, Mohammad Hassan Karimi, -1

机译：使用PIV技术以低雷诺数在具有基本空腔的厚钝尾缘翼型上进行流动可视化
7. Aerodynamic and Aeroacoustic Performance of Airfoils Fitted with Morphing Trailing-edges [O] . Hasan Kamliya Jawahar, Qing Ai, Mahdi Azarpeyvand 2018

机译：适用于变形后边缘的翼型的空气动力学和空气声性能
8. Low-speed investigation of the aerodynamic loads on the droop-nose flap of a wing with leading edge swept back 47.5 degrees and having symmetrical circular-arc airfoil sections at a Reynolds number of 4.3 x 10 (exp 6) [R] . Whittle, Edward F , Jr, Fink, Marvin P 1950

机译：低速研究机翼下垂翼片上的空气动力载荷，前缘向后扫47.5度，雷诺数为4.3×10（exp 6）时具有对称的圆弧翼型截面

Combined droop nose and trailing-edges morphing effects on airfoils aerodynamics

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