Method for obtaining static aeroelastic deformation influencing quantity of wind tunnel model
A technology of static aeroelasticity and influence quantity, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve the problems of inability to realize real-time data analysis, high time and calculation costs, reliability dependence, etc., to avoid Test the scrapping of trains, reduce the difficulty and preparation period, and reduce the effect of dependence
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[0026] In order to clearly illustrate the technical features of the solution, the solution will be described below through a specific implementation mode combined with the accompanying drawings.
[0027] In the wind tunnel test, without considering the changes of other parameters (such as Mach number Ma, model angle of attack α), the aerodynamic coefficient C under the elastic shape f,elastic It can be expressed as a function of Reynolds number Re and incoming flow velocity and pressure q
[0028] C f,elastic = f(Re,q) (1)
[0029] The existence of flow velocity pressure will cause the static elastic deformation of the wing structure of the wind tunnel model, so the aerodynamic coefficient can be divided into the rigid shape aerodynamic coefficient C f,rigid The change of aerodynamic coefficient ΔC caused by the static aeroelastic deformation of the wing f,elastic Two parts, where C f,rigid Only varies with Re, ΔC f,elastic With the change of Re and q, the formula can be ...
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