甲板发射乘波器配置飞机的概念设计

Conrad F. Newberry
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引用次数: 3

摘要

为了评估巡航马赫数在3≤M∞≤5范围内设计的舰载战术乘波机的可行性,对五个研究生课堂设计团队的成果进行了回顾。设计团队的努力表明,这种飞机的作战半径可能达到580nm / 1500nm。支持这种飞机发展的低速研究表明,在亚音速飞行状态下,乘波机平台可能是静态不稳定的,与类似的简单三角翼平台相比,乘波机配置的旋涡升力可能更弱,升力、阻力和俯仰力矩数据在较大的迎角范围内(如图所示的- 20°≤α≤20°数据)表现良好。
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The conceptual design of deck-launched waverider-configured aircraft

The results of five graduate classroom design teams are reviewed in order to assess the feasibility of carriercapable tactical waverider-configured aircraft designed for cruise Mach numbers in the range 3≤M≤5. The efforts of the design teams suggests that such aircraft are probably feasible for combat radii of 580nm<R<1500nm. Low-speed research to support the development of such aircraft indicates that within the subsonic flight regime, waverider planforms may be statically unstable, vortex lift may be less strong for waverider configurations than for similar simple delta wing planforms and lift, drag and pitching moment data appear to be well behaved within a large (−20°≤α≤20° data shown herein) angle-of-attack range.

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