Aerodynamic layout design method based on variable-configuration aerospace vehicle
An aerospace vehicle and aerodynamic layout technology, which is applied to aircraft parts, ground devices, transportation and packaging, etc., can solve problems such as great difficulty in engineering realization, to ensure system stability and maneuverability, optimize flight performance, The effect of improving aerodynamic performance
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[0050] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.
[0051] Such as figure 1 Shown is an aerodynamic layout design method based on a variable configuration aerospace vehicle, including the following steps:
[0052] Step 1: Build a parametric geometric model
[0053] Determine the low-speed reference layout and high-speed reference layout of the variable-configuration aerospace vehicle respectively, and use the state type function method to parametrically describe the geometric shape of the variable-configuration aerospace vehicle; The geometric parameters of its shape features, and determine whether these parameters are completely independent and the constraints between the parameters, obtain a complete geometric parameter set that can describe the aircraft, and then specify the value of the parameter set, and use the component disassembly method to generate a specific aircraft shape.
[0054] As shown ...
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