Observation system and method for aerodynamic force test and flapping wing flow field of flapping-wing micro air vehicle
A technology of a flapping aircraft and an observation system, which is applied in the aerospace field, can solve the problems of less experimental equipment for a micro flapping aircraft, restricting the research and development of the flapping aircraft, and less experimental data for the flapping aircraft, etc. High practical performance and comprehensive data effect
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[0038] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments. This embodiment is carried out on the premise of the technical solution of the present invention, and detailed implementation and specific operation process are given, but the protection scope of the present invention is not limited to the following embodiments.
[0039] Such as Figure 1 ~ Figure 3 As shown, the present invention provides a micro flapping-wing aircraft aerodynamic testing and flapping-wing flow field observation system, which mainly includes: flapping-wing aircraft 5, aerodynamic testing device, and three-dimensional particle image velocimetry device. The aerodynamic test device mainly includes a six-dimensional force sensor 10, an angle sensor 13, a diffuse reflection switch 2, a data collector 8, and a host computer 9. The three-dimensional particle image velocity measurement device mainly includes: tracer particles, laser ...
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