Citation: | Huang Da, Li Zhiqiang, Wu Genxing. Study of Data Expression and Mathematical Modelling for Unsteady Experiment of a Model Pitching in Large Amplitude[J]. ACTA AERODYNAMICA SINICA, 1999, 17(1): 68-72. |
[1] | Guo Li, Lyu Jinan, Feng Feng, Wang Qiang. CFD verification and weak compressibility correction of unsteady aerodynamic force models applied to high-amplitude oscillating incoming flows[J]. ACTA AERODYNAMICA SINICA, 2017, 35(1): 93-100. DOI: 10.7638/kqdlxxb-2015.0065 |
[2] | 白俊强, 李鑫, 华俊, 王昆. 过冷大水滴情况下的积冰数值模拟[J]. ACTA AERODYNAMICA SINICA, 2013, 31(6): 801-811. |
[3] | SHI Zhi-wei, WU Gen-xing, HUANG Da. The validation of unsteady aerodynamic model based on the high amplitude harmonic rolling motion test[J]. ACTA AERODYNAMICA SINICA, 2010, 28(6): 650-654. |
[4] | WANG Wen-zheng, GUI Ye-wei, HE Kai-feng, YUAN Xian-xu, CHEN Yan-qin. Aerodynamic data fusion technique exploration[J]. ACTA AERODYNAMICA SINICA, 2009, 27(5): 524-528. |
[5] | HUANG Da, ZHENG Sui, WEN Li-hong, WU Gen-xin. Investigation on contain of the large amplitude test to the general dynamic derivative test[J]. ACTA AERODYNAMICA SINICA, 2008, 26(1): 111-114. |
[6] | HUANG Da, WU Gen-xing. Investigation of the unsteady aerodynamic characteristics for a fighter rolling in large amplitude[J]. ACTA AERODYNAMICA SINICA, 2005, 23(2): 135-138. |
[7] | HUANG Da, LI Zhi-qiang, SHI Zhi-wei, WU Gen-xing. A Nonlinear Stability Analysis for an Aircraft Rolling in Large Amplitude Motion[J]. ACTA AERODYNAMICA SINICA, 2000, 18(4): 401-406. |
[8] | DING Ke-wen, ZHANG Wen-hua, Li Zhi-qiang, QI Meng-bu, REN Rong-sheng. The Research of Wall Interference on Unsteady Pressure Tests for Dalta Wing Undergoing Large Amplitude Pitching Motions[J]. ACTA AERODYNAMICA SINICA, 2000, 18(3): 330-335. |
[9] | Shi Zhiwei, Wu Genxing. The Comparison of Several Unsteady Aerodynamics Models at High Angle of Attack[J]. ACTA AERODYNAMICA SINICA, 1999, 17(4): 452-460. |
[10] | Huang Da, Li Zhiqiang, Wu Genxing. Dynamic Derivative Simulation and Mathematical Model of the Wind Tunnel Test about a Model Pitching in very Large Amplitude[J]. ACTA AERODYNAMICA SINICA, 1999, 17(2): 219-223. |