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System and method for calculating aerodynamic performance of tilting wing aircraft
System and method for calculating aerodynamic performance of tilting wing aircraft
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机译:用于计算倾斜翼飞机的空气动力性能的系统和方法
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摘要
Aerodynamic performance parameters for aircraft configurations are calculated using an aerodynamic performance system and method. The aerodynamic performance system in a workstation includes a processor circuit having a processor and a memory. Additionally, the system includes aerodynamic performance logic stored on the memory and executable by the processor. The aerodynamic performance logic includes logic that calculates a number of aerodynamic performance parameters for a configuration. Further, the logic generates an aerodynamic performance report to be sent to a client via a network. The aerodynamic performance report lists at least one of the aerodynamic performance parameters.
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