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AEROWING: The Software for Aerodynamic Analysis of a Large Aspect-Ratio FiniteWing at Low Speeds

机译:aEROWING:低速下大纵横比有限元空气动力学分析软件

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摘要

An existing computer software package for the determination of lift, drag, andpitching moment of the finite wing is ported onto PS 386/387 system and validated against known examples. This software, is presently designated as AEROWING and is used to obtain the loads on the wing of an remotely piloted vehicle. The results prove that the software can provide a tool for the wing analysis and design.

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