journal article Sep 01, 1997

Hysteresis of a separated variable-velocity flow about a straight-wing model

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References
8
[1]
A. I. Kur'yanov, G. I. Stolyarov, and R. I. Steinberg, “Hysteresis of aerodynamic characteristics,”Uch. Zap. TsAGI,10, No. 3, 12–15 (1979).
[2]
V. Ya. Neiland, G. I. Stolyarov, and V. G. Tabachnikov, “The effect of the relative thickness of a rectangular wing with low aspect ratio and Reynolds number on flow-structure rearrangement regimes,”Uch. Zap. TsAGI,16, No. 3, 1–10 (1985).
[3]
Yu. A. Kolmakov, Yu. A. Ryzhov, G. I. Stolyarov, and V. G. Tabachnikov, “The flow structure about a rectangular wing λ=5 at high angles of attack,”Tr. TsAGI, No. 2290, 84–89 (1985).
[4]
B. Yu. Zanin, V. V. Kozlov, and V. N. Lushin, “Flow separation control on a straight and swept wing by acoustic action,”Sib. Fiz.-Tekh. Zh., No. 3, 32–36 (1992).
[5]
V. N. Lushin, “The flow about a finite-span wing under external acoustic effect,”Sib. Fiz.-Tekh. Zh., No. 4, 64–68 (1992).
[6]
V. V. Kozlov, F.-R. Grosche, A. V. Dovgal, et al., “Control of Leading-Edge Separation by Acoustic Excitation,” Report No. 222-93, DLR, Goettingen (1993).
[7]
A. V. Boiko, A. V. Dovgal', B. Yu. Zanin, et al., “Topology of global separation on an airfoil in the presence of a source of stationary disturbances,”Teplofiz. Aeromekh.,2, No. 1, 37–45 (1995).
[8]
A. E. Winkelmann and J. B. Barlow, “A flowfield model for a rectangular planform wing beyond stall,”AIAA J.,18, No. 8, 1006–1008 (1980). 10.2514/3.50846
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Published
Sep 01, 1997
Vol/Issue
38(5)
Pages
724-727
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Cite This Article
B. Yu. Zanin (1997). Hysteresis of a separated variable-velocity flow about a straight-wing model. Journal of Applied Mechanics and Technical Physics, 38(5), 724-727. https://doi.org/10.1007/bf02467884
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