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Aerodynamic effects of oversized tires and tall landing gear on a small general aviation aircraft

机译:超大地轮胎和高落地齿轮在小型通用航空飞机上的空气动力学效应

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An experimental investigation was conducted to identify the aerodynamic effects of oversized low-pressure (Tundra) tires and tall landing gear on a Piper Super Cub airplane. Water tunnel and wind tunnel tests were performed using, respectively, a 1/20 scale model and full-scale landing gear and tire components. Force and moment data suggest that larger tires and taller gear most affect the drag and side force. Small trim changes are apparent, but the basic static stability behavior appears unchanged.
机译:进行了实验研究,以确定超大压(TUNDRA)轮胎和高着陆齿轮在吹笛式超级幼崽飞机上的空气动力学效应。 分别使用1/20级模型和全尺寸起落架和轮胎部件进行水隧道和风洞测试。 力量和时刻数据表明,较大的轮胎和较高的装备最大地影响了阻力和侧力。 小修剪变化很明显,但基本的静态稳定行为出现不变。

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