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Ando, S.; Yamamoto, Y.

Induced drag of a straight wing in a wind tunnel of circular cross section. (English) Zbl 0343.76001

Ing.-Arch. 45, 161-170 (1976).
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MSC:

76B10 Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing
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References:

[1] Rosenhead, L.: The effect of wind tunnel interference on the characteristics of an aerofoil. Proc. Roy. Soc. A. Vol. 129 (1930) pp. 135-145 · JFM 56.1261.01 · doi:10.1098/rspa.1930.0147
[2] Millikan, C. B.: On the lift distribution for a wing of arbitrary plan form in a circular wind tunnel. Trans. ASME, APM-54-19 (1932) pp. 197-203
[3] Tani, I.; Taima, M.: Two notes on the boundary influence of wind tunnels of circular cross section. Report of Aeron. Res. Inst. Tokyo Imp. Univ. No. 121, June 1935
[4] Barrows, T. M.: Widnal, S. E.: Optimum lift-drag ratio for a ram wing tube vehicle. AIAA J. 8 (1970), pp. 491-497 · doi:10.2514/3.5695
[5] Ando, S.: An idealized ground effect wing. Aeron. Quart. 17 (1966) pp. 53-71
[6] Mamada, H.; Ando, S.: Minimum induced drag of a hemi-circular ground effect wing. J. Aircraft (1973) pp. 660-663
[7] Yamamoto, Y.: Optimum lift distribution of a hemi-circular ground effect wing. J. Japan Soc. Aeron. Space Sci. 23, No. 259 (1975) pp. 480-483 (in Japanese)
[8] Byrd, P. F.; Friedman, M. D.: Handbook of elliptic integrals for engineers and physicists. Berlin-Göttingen-Heidelberg 1954 · Zbl 0055.11905
[9] Van Dyke, M. D.: Perturbation methods in fluid mechanics. New York 1964 · Zbl 0136.45001
[10] Gradshteyn, I. S.; Rhyzik, I. M.: Tables of Integrals, Series and Products. New York 1965
[11] Ando, S.: Limitation of lifting line theory for wing having very small chordwise gap. Trans. Japan. Soc. Aero. Space. Sci. 9, No. 14 (1966) pp. 1-110
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