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AN AUTOMATED APPROACH TO NACELLE PARAMETERIZATION USING INTUITIVE CLASS SHAPE TRANSFORMATION CURVES

机译:使用直观类形状转换曲线的纳赛尔参数化自动方法

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A tool to create parametric aerodynamic shapes using intuitive design variables based on class shape transformation curves is presented. To enable this, a system has been developed which accepts arbitrary constraints and automatically derives the analytical expressions which describe the corresponding class shape transformation curves. Parametric geometry definitions for fan cowl and intake aero-lines were developed using the generalized method. CFD analysis of the fan cowl shows that despite the simple geometry definition its performance characteristics are close to what would be expected of a finished design. The intake geometry was generated in a similar way and met the typical performance metrics for conventional intakes. This demonstrates the usefulness of the tool to quickly and robustly produce parametric aero-lines with good aerodynamic properties, using relatively simple intuitive design variables.
机译:提出了使用基于类形状转换曲线的直观设计变量来创建参数空气动力形状的工具。为了实现这一点,已经开发了一个系统,该系统接受任意约束,并自动派生描述相应的类形状变换曲线的分析表达式。使用广义方法开发了风扇罩和摄入气线的参数几何定义。 CFD分析风扇COWL表明,尽管几何定义简单,其性能特征靠近预期的成品设计。进气几何形状以类似的方式产生,并达到常规摄入量的典型性能度量。这证明了工具能够快速且强大地产生具有良好空气动力学性能的参数化航空线的有用性,使用相对简单的直观设计变量。

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