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Identification of aircraft longitudinal aerodynamic parameters using an online corrective test for wind tunnel virtual flight
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作者 Shang TAI Chen BU +3 位作者 Yanling WANG Ting YUE Hailiang LIU Lixin WANG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2024年第9期261-275,共15页
The identification of aerodynamic parameters is accomplished through the test data of the dynamic movement of scaled aircraft models flying dynamically in wind tunnel,which can real-ize the accurate acquisition of the... The identification of aerodynamic parameters is accomplished through the test data of the dynamic movement of scaled aircraft models flying dynamically in wind tunnel,which can real-ize the accurate acquisition of the aerodynamic model of the aircraft in the preliminary stage for aircraft design,and it is of great significance for improving the efficiency of aircraft design.How-ever,the translational motion of the test model in the wind tunnel virtual flight is subject to con-straints that result in distinct flight dynamics compared to free flight.These constraints have implications for the accuracy of aerodynamic derivatives obtained through the identification of wind tunnel test data.With this issue in mind,the research studies the differences in longitudinal dynamic characteristics between unconstrained free flight and wind tunnel virtual flight,and inno-vatively proposes an online correction test based wind tunnel virtual flight test technique.The lon-gitudinal trajectory and velocity changes of the model are solved online by the aerodynamic forces measured during the test,and then the coupled relationship between aircraft translation and rota-tion is used to correct the model's pitch attitude motion online.For the first time,the problem of solving the data approximation for free flight has been solved,eliminating the difference between the dynamics of wind tunnel virtual flight and free flight,and improving the accuracy of the aero-dynamic derivative identification results.The experiment's findings show that accurate aerodynamic derivatives can be identified based on the online correction test data,and the observed behaviour of the identified motion model has similarities to that of the free flight motion model. 展开更多
关键词 Wind tunnels Displacement constraints online solution Flightcontrol law Aerodynamic parameter identification
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Take Advantage of Multimedia for Medical English Teaching
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作者 Gong Chen 《Sino-US English Teaching》 2005年第2期47-50,共4页
This paper is my humble opinion on why multimedia should be integrated into the teaching of English for medical purpose (EMP) and how we can make the best use of IT (information technology) in EMP teaching. By com... This paper is my humble opinion on why multimedia should be integrated into the teaching of English for medical purpose (EMP) and how we can make the best use of IT (information technology) in EMP teaching. By combining large amount of medical resources with the content of textbook, computerize teaching material can be produced In which, graphics, pictures as well as animations and flashes are used to present ideas, demonstrate "hard-to-understand" concepts, and more, links provided to explore current data on the web concerning given medical knowledge. It is shown here the multimedia environment provides us a new and desirable approach to enhance the delivery and interactivity of medical linguistic course. 展开更多
关键词 multimedia EMP IT (information technology) flash animations graphics commercial VCD and CD Webs-based teaching solutions online resources
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