QUANTITATIVE LOW-SPEED WAKE SURVEYS

被引:47
作者
BRUNE, GW
机构
[1] Boeing Commercial Airplane Group, Seattle, WA
来源
JOURNAL OF AIRCRAFT | 1994年 / 31卷 / 02期
关键词
Wakes;
D O I
10.2514/3.46481
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Theoretical and practical aspects of conducting three-dimensional wake measurements in large wind tunnels are reviewed with emphasis on applications in low-speed aerodynamics. Such quantitative wake surveys furnish separate values for the components of drag such as profile drag and induced drag, but also measure lift without the use of a balance. In addition to global data, details of the wake flowfield as well as spanwise distributions of lift and drag are obtained. This article demonstrates the value of this measurement technique using data from wake measurements conducted on a variety of low-speed configurations including the complex high-lift system of a transport aircraft.
引用
收藏
页码:249 / 255
页数:7
相关论文
共 22 条
  • [11] Batchelor G.K., Axial Flow in Trailing Line Vortices, Journal of Fluid Mechanics, 20, pp. 645-653, (1964)
  • [12] El-Ramly Z., Rainbird W.J., Earl D.G., Wind Tunnel Measurements of Rolling Moment in a Swept-Wing Vortex Wake, Journal of Aircraft, 13, 12, pp. 962-967, (1976)
  • [13] El-Ramly Z.M., Rainbird W.J., Effect of Simulated Jet Engines on the Flowfield Behind a Swept-Back Wing, Journal of Aircraft, 14, 4, pp. 343-349, (1977)
  • [14] El-Ramly Z.M., Rainbird W.J., Computer-Controlled System for the Investigation of the Flow Behind Wings, Journal of Aircraft, 14, 7, pp. 668-674, (1977)
  • [15] El-Ramly Z.M., Rainbird W.J., Flow Survey of the Vortex Wake Behind Wings, Journal of Aircraft, 14, 11, pp. 1102-1108, (1977)
  • [16] Van Dam C.P., Nikfetrat K., Chang I.C., Vijgen P.M.H.W., Drag Calculations of Wings Using Euler Methods, (1991)
  • [17] Schwarztrauber P.N., Sweet R.A., Efficient Fortran Subprograms for the Solution of Separable Elliptic Partial Differential Equations, Association of Computing Machinery Transactions of Mathematical Software, 5, 3, pp. 352-364, (1979)
  • [18] Rae W.H., Pope A., Low Speed Wind Tunnel Testing, (1984)
  • [19] Brune G.W., Hallstaff T.H., Wing Span Loads of Complex High-Lift Systems from Wake Measurements, Journal of Aircraft, 22, 9, pp. 831-832, (1985)
  • [20] Tinoco E.N., CFD Applications to Complex Configurations: A Survey, Applied Computational Aerodynamics, 125, pp. 559-584, (1990)