原文传递
Preliminary Investigation at Low Speeds of Swept Wings in Rolling Flow
| 题名： | Preliminary Investigation at Low Speeds of Swept Wings in Rolling Flow |
| 作者： | Feigenbaum, D., Goodman, Alex |
| 关键词： | *AIR FLOW, SWEPTBACK WINGS, AERODYNAMIC FORCES |
| 摘要： | Investigation is made to determine characteristics of untapered wings with various angles of sweepback under conditions simulating straight and rolling flow. Characteristics of aileron on 45 Degrees swept-back wing are given. Results of test in straight flow correspond with previously obtained results. Lateral-force coefficient varies with wing tip helix angle in rolling flow. Damping in roll becomes more negative with increasing lift coefficient. |
| 总页数： | 39 |
| 报告类型： | 科技报告 |
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