摘要: Subsonic lateral-direction and longitudinal characteristics of a forward-swept-wing fighter configuration were examined in wind-tunnel tests at Mach numbers of 0.2 and 0.5 for angles of attack from -7 to 47 deg. and over a sidelsl... 展开
作者 | mann, m. j. huffman, j. k. | ||
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原报告号 | N8726874 | 总页数 | 103 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aerodynamic configurations Angle of attack Fighter aircraft Lateral stability Subsonic aircraft Swept forward wings Lateral control Canard configurations Flaps (Control surfaces) Leading edges Mach number Sideslip Strakes Trailing edges Wind tunnel tests |