Displacement element for wind tunnel pitching dynamic derivative test and design method of displacement element
A technology of displacement components and design methods, applied in aerodynamic tests, design optimization/simulation, special data processing applications, etc. The effect of waste, saving resources, and expanding test capacity
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[0061] This embodiment adopts the design method of the displacement element for the wind tunnel pitch dynamic derivative test of the present invention, and completes the following Figure 4 The design of the displacement element is shown. The specific parameters of the displacement element are as follows:
[0062] Maximum diameter D = 66mm; cross beam length L = 50mm; cross beam angle φ = 50°; amplitude θ = 0.8°; distance between adjacent single measuring beams δ = 1.0mm; b3=b4=14mm; design thickness of the cross beam h=8mm; measure the strain value of the beam ε 仿真 ≈453×10 -6 . Figure 4 EPSX in represents the strain along the X direction, and the strain meets the test requirements.
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