摘要: A 0.237-scale model of a remotely piloted research vehicle equipped with a thick, high-aspect-ratio supercritical wing was tested in the Langley 8-foot transonic tunnel to provide experimental data for a prediction of the static s... 展开
作者 | Byrdsong, T. A. Brooks, C. W. | ||
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原报告号 | N83-11142 | 总页数 | 218 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Directional stability Lateral control Longitudinal control Remotely piloted vehicles Supercritical wings Wind tunnel tests Control stability Lateral stability Longitudinal stability Scale models Slender wings Static stability |