摘要: This investigation is a continuation of the experimental and theoretical evaluation of blended wing-body combinations. The basic diamond, delta, and arrow plan forms which had an aspect ratio of 2 with leading-edge sweeps of 45.00... 展开
作者 | Holdaway, G. H. Mellenthin, J. A. | ||
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原报告号 | N19980223980 | 总页数 | 80 |
主办者 | National Aeronautics and Space Administration | ||
报告分类号 | [51A - Aerodynamics] | ||
报告类别/文献类型 | DE / NTIS科技报告 | ||
关键词 | Body-wing configurations Cambered wings Twisted wings Aerodynamic coefficients Airfoil profiles Subsonic speed Transonic speed Supersonic speed Mach number Aspect ratio Aerodynamic drag Loads(Forces) Leading edges Thickness Wave drag Wing camber Zero lift |