Calculation and Measurement of Induced Drag at Low Speeds
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C. P. van Dam | P. M. H. W. Vijgen | C. M. Fremaux | C. P. Dam | P. Vijgen | K. Nikfetrat | K. Nikfetrat
[1] Induced drag and the ideal wake of a lifting wing , 1989 .
[2] C. P. van Dam,et al. Sheared Wing-Tip Aerodynamics: Wind-Tunnel and Computational Investigation , 1989 .
[3] Arthur Fage,et al. An Investigation of the Air-Flow Pattern in the Wake of an Aerofoil of Finite Span , 1926 .
[4] C. P. van Dam,et al. Induced-drag characteristics of crescent-moon-shaped wings , 1987 .
[5] J. W. Slooff,et al. Aircraft drag prediction and reduction. Addendum 1: Computational drag analyses and minimization; mission impossible? , 1986 .
[6] James Crowder. Flow visualization in flight testing , 1990 .
[7] E. C. Maskell,et al. Progress towards a method for the measurement of the components of the drag of a wing of finite span , 1972 .
[8] J. E. Yates,et al. A fundamental study of drag and an assessment of conventional drag-due-to-lift reduction devices , 1986 .
[9] Martin V. Lowson,et al. Minimum Induced Drag for Wings with Spanwise Camber , 1990 .
[10] Max M Munk,et al. The Minimum Induced Drag of Aerofoils , 1979 .
[11] C. P. van Dam,et al. Wind-tunnel investigation on the effect of a crescent planform on drag , 1990 .
[12] James Chen-yuan Wu,et al. A generalized wake-integral approach for drag determination in three-dimensional flows , 1979 .
[13] Thomas H. Pulliam,et al. Navier-Stokes computations for exotic airfoils , 1985 .
[14] C. D. Cone,et al. THE THEORY OF INDUCED LIFT AND MINIMUM INDUCED DRAG OF NONPLANAR LIFTING SYSTEMS , 1962 .
[15] Mark Dehaan. Induced drag of wings with highly swept and tapered wing tips , 1990 .
[16] C. W. Burkett. Reductions in induced drag by the use of aft swept wing tips , 1989, The Aeronautical Journal (1968).
[17] Brian Maskew,et al. Prediction of Subsonic Aerodynamic Characteristics: A Case for Low-Order Panel Methods , 1982 .
[18] W. R. Sears. On Calculation of Induced Drag and Conditions Downstream of a Lifting Wing , 1974 .