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Progressive Aerodynamic Model Identification from Dynamic Water Tunnel Test of the F- 16XL Aircraft

机译：从F-16XL飞机的动态水隧道试验获得的渐进式空气动力学模型识别

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《AIAA Atmospheric Flight Mechanics Conference and Exhibit》|2004年|P.1-20|共20页
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作者
P. Murphy; V. Klein; N. Szyba;
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中图分类航空仪表、航空设备、飞行控制与导航;
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专利

1. Wind-Tunnel Aerodynamics in Rotary Tests of Combat Aircraft Models [J] . Lars E. Ericsson, Martin E. Beyers Journal of Aircraft . 1998,第4期

机译：战斗机模型旋转试验中的风洞空气动力学
2. Identification of Fixed-Wing Micro Aerial Vehicle Aerodynamic Derivatives from Dynamic Water Tunnel Tests [J] . Krzysztof Sibilski, Miros?aw Nowakowski, Dariusz Rykaczewski, Aerospace . 2020,第8期

机译：动态水隧道试验识别固定翼微空气车辆空气动力学衍生物
3. Commuter aircraft aerodynamic characteristics through wind tunnel tests [J] . Nicolosi Fabrizio, Corcione Salvatore, Della Vecchia Pierluigi Aircraft engineering . 2016,第4期

机译：通过风洞测试的通勤飞机空气动力学特性
4. Evaluation and Analysis of F- 16XL Wind Tunnel Data from Dynamic Tests [C] . S. Kim, P. Murphy, V. Klein AIAA Guidance, Navigation, and Control Conference and Exhibit ; AAS Astrodynamics Specialist Conference ; AIAA Atmospheric Flight Mechanics Conference and Exhibit ; AIAA Modeling and Simulation Technologies Conference and Exhibit . 2003

机译：F-16XL风洞数据动态测试评估与分析
5. MAXIMUM LIKELIHOOD IDENTIFICATION OF AIRCRAFT PARAMETERS WITH UNSTEADY AERODYNAMIC MODELLING. [D] . KESKAR, DINESH ACHYUT. 1979

机译：具有非定常气动模型的飞机参数的最大似然识别。
6. Aircraft Aerodynamic Parameter Detection Using Micro Hot-Film Flow Sensor Array and BP Neural Network Identification [O] . Ruiyi Que, Rong Zhu 2012

机译：微型热膜流量传感器阵列和BP神经网络识别的飞机气动参数检测
7. Progressive Aerodynamic Model Identification From Dynamic Water Tunnel Test of the F-16XL Aircraft [O] . Patrick C. Murphy, Vladislav Klein, Nathan M. Szyba 2008

机译：从F-16XL飞机的动态水隧道试验获得渐进的空气动力学模型识别
8. Progressive Aerodynamic Model Identification From Dynamic Water Tunnel Test of the F-16XL Aircraft [R] . Murphy, Patrick C., Klein, Vladislav, Szyba, Nathan M. 2004

机译：F-16XL飞机动态水隧道试验的渐进气动模型识别

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