Abstract
Measurements on a large circular cylinder in a pressurized wind tunnel at Reynolds numbers from 106 to 107 reveal a high Reynolds number transition in which the drag coefficient increases from its low supercritical value to a value 0.7 at R = 3.5 × 106 and then becomes constant. Also, for R > 3.5 × 106, definite vortex shedding occurs, with Strouhal number 0.27.
Publisher
Cambridge University Press (CUP)
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Reference16 articles.
1. Millikan, C. B. 1957 Advanced education and academic research in aeronauties. J. R. Aero. Soc. 61, 793–808.
2. Eppler, R. 1954 Beiträge zu Theorie und Anwendung der unstetigen Strömungen. J. Rational Tech. Anal. 3, 591–644.
3. Fung, Y. C. 1960 Fluctuating lift and drag acting on a cylinder in a flow at supereritical Reynolds numbers. J. Aero Space Sci. 27, 801–14.
4. Ribner, H. S. & Etkin, B. 1958 Noise research in Canada. Proc. 1st Int. Congr. Aero. Sci., Madrid (publ. by Pergamon Press, London, 1959).
5. Dryden, H. L. & Hill, G. C. 1930 Wind pressure on circular cylinders and chimneys. Bur. Stand. J. Res., Wash., 5, 653–93.
Cited by
1047 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献