摘要: The results of a wind tunnel test to investigate the controlling effects of tangential, leading edge blowing on the vortical flow over a delta wing are given. Blowing is used to directly control the crossflow separation points at ... 展开
作者 | Wood, N. J. Roberts, L. | ||
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原报告号 | N86-30094 | 总页数 | 73 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Cross flow Delta wings Leading edges Wind tunnel tests Lift augmentation Vortices Aerodynamic coefficients Angle of attack Pressure distribution |