摘要: The expanded capabilities for analysis and design of low speed flap systems afforded by recent modifications of an existing computer program is described. The program provides for the simultaneous analysis of up to 25 pairs of lea... 展开
作者 | Carlson, H. W. Walkley, K. B. | ||
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原报告号 | NASA-CR-3675 | 总页数 | 75 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | AERODYNAMIC COEFFICIENTS COMPUTER PROGRAMS DESIGN ANALYSIS LOW SPEED SUBSONIC FLOW WING FLAPS ARROW WINGS LEADING EDGE FLAPS MACH NUMBER REYNOLDS NUMBER SUPERSONIC AIRCRAFT TRAILING EDGE FLAPS VORTICES WIND TUNNEL TESTS |