Micro flapping-wing analysis system and method involved with pneumatic and structural coupling properties
An analysis system and characteristic analysis technology, applied in the field of micro flapping wing analysis system, can solve the problems of inability to fully consider the coupling effect of flexible flapping wing aerodynamic structure, low accuracy, poor solution convergence, etc. effect of reference
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[0029] Describe the present invention below in conjunction with specific embodiment:
[0030] Refer to attached figure 1 , the micro-flapping wing analysis system in this embodiment considering the aerodynamic and structural coupling characteristics consists of a main control computer, a server, a structural static characteristic testing system, a structural dynamic characteristic testing system, an aerodynamic response analysis system, a structural response analysis system and a coupling characteristic Analysis system composition; hardware devices are connected by 100M optical fiber. When executing, firstly, the main control computer issues commands to control the structural static characteristic test system (3), and measure the static structural characteristics of the micro-flapping wing. The specific description is as follows: figure 2 shown. Secondly, the main control computer controls the structural dynamic characteristic test system (4), and the measured dynamic struc...
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