原文传递
Effects of a Fuselage and Various High-Lift and Stall-Control Flaps on Aerodynamic Characteristics in Ptich of an NACA 64 Series 40 Degree Swept-Back Wing
| 题名： | Effects of a Fuselage and Various High-Lift and Stall-Control Flaps on Aerodynamic Characteristics in Ptich of an NACA 64 Series 40 Degree Swept-Back Wing |
| 作者： | Connor, D. W., Neely, Robert H. |
| 关键词： | *SWEPTBACK WINGS, AERODYNAMIC CONTROL SURFACES, AERODYNAMIC FORCES, FLAPS(CONTROL SURFACES) |
| 摘要： | Wind-tunnel tests were carried out to determine low-speed lift, drag, and pitching moment of the wing tested alone, with various flaps, and in various combinations with the fuselage having 10.2:1 fineness ratio. The results are given in graphs. Rolling-moment characteristics are included in some instances. The locations of aerodynamic centers are given for some configurations and for various wing-fuselage combinations. The table gives characteristics for Reynolds No. 6,840,000 for comparing effects of various flaps. NOTE: Requests for copies of this report must be addressed to: N.A.C.A., Washington, DC |
| 总页数： | 50 |
| 报告类型： | 科技报告 |
相关文献
- Preliminary Investigation at Low Speeds of Swept Wings in Rolling Flow
- Simulation Modeling Requirements for Loss-of-Control Accident Prevention of Turboprop Transport Aircraft.
- An airfoil for general aviation applications
- Assessment of a Conceptual Flap System Intended for Enhanced General Aviation Safety
- Continuous Trailing-Edge Flaps for Primary Flight Control of a Helicopter Main Rotor.
- Super Cooled Large Droplet Analysis of Several Geometries Using LEWICE3D Version 3.
检索历史
应用推荐
