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Evaluation and further analysis of unsteady pressure response measurements on an airfoil at angle of attack

机译：评价及进一步分析攻角翼型翼型的不稳定压力响应测量

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《American Institute of Aeronautics and Astronautics/Corporate Emergency Access System Aeroacoustics Conference Exhibit》|2002年||共23页
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1. Uncertainty analysis of motion-capturing pressure-sensitive paint method based on unsteady surface-pressure measurement on fluttering airfoil [J] . Kurihara Daiki, Saitoh Kenichi, Sakaue Hirotaka Aerospace science and technology . 2020,第Auga期

机译：基于非定常表面压力测量的运动捕获压敏涂料方法的不确定性分析
2. Input-output reduced-order modeling of unsteady flow over an airfoil at a high angle of attack based on dynamic mode decomposition with control [J] . Sun Chong, Tian Tian, Zhu Xiaocheng, International Journal of Heat and Fluid Flow . 2020,第Deca期

机译：基于动态模式分解的基于动态模式分解，在翼型中对翼型的输入输出减小阶数模型。
3. Unsteady airloads on static airfoils through high angles of attack and in reverse flow [J] . Lind Andrew H., Jones Anya R. Journal of Fluids and Structures . 2016,第Null期

机译：静态翼型上的不稳定载荷会通过大迎角和反向流动而产生
4. Evaluation and further analysis of unsteady pressure response measurements on an airfoil at angle of attack [C] . P. Mish, W. Devenport 8th AIAA/CEAS Aeroacoustics Conference amp; Exhibit . 2002

机译：评价和进一步分析机翼迎角非定常压力响应的测量结果
5. Hot-film measurements of the steady and unsteady boundary layer development on a low-pressure turbine airfoil. [D] . Zhang, Xuefeng. 2002

机译：低压涡轮机翼片上稳定和非稳定边界层发展的热膜测量。
6. Analysis of pressure angle and temporal effects on tissue optical properties from polarization-gated spectroscopic probe measurements [O] . Sarah Ruderman, Andrew J. Gomes, Valentina Stoyneva, 2010

机译：通过偏振门控光谱探针测量分析压力角度和时间对组织光学特性的影响
7. Unsteady Separated Flows around Airfoils at High Attack Angles. [O] . Takahiko TANAHASHI, Junsuke OMI, Yasumasa KATO, 1991

机译：在高攻击角处的翼型周围的不稳定分离流。
8. Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack [R] . Nallasamy, M., Groeneweg, J. F. 1989

机译：预测先进螺旋桨在迎角处的非定常叶片表面压力

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