A natural low-frequency oscillation of the flow over an airfoil near stalling conditions
暂无分享,去创建一个
[1] Donald E. Gault,et al. Examples of three representative types of airfoil-section stall at low speed , 1951 .
[2] W. Farren,et al. THE REACTION ON A WING WHOSE ANGLE OF INCIDENCE IS CHANGING RAPIDLY WIND TUNNEL EXPERIMENTS WITH A SHORT PERIOD RECORDING BALANCE , 1935 .
[3] Khairul Q. Zaman,et al. Turbulence suppression in free shear flows by controlled excitation , 1981, Journal of Fluid Mechanics.
[4] J. C. Townsend,et al. Computation and analysis of a cylinder wake flow , 1987 .
[5] Khairul Q. Zaman,et al. Taylor hypothesis and large-scale coherent structures , 1981, Journal of Fluid Mechanics.
[6] A. Roshko. On the drag and shedding frequency of two-dimensional bluff bodies , 1954 .
[7] D. J. Mckinzie,et al. Control of laminar separation over airfoils by acoustic excitation , 1989 .
[8] W. D. Harvey,et al. Transition and separation control on a low-Reynolds number airfoil , 1986 .
[9] R. Parker,et al. Resonance effects in wake shedding from parallel plates: Some experimental observations , 1966 .
[10] K. Zaman,et al. Effect of acoustic excitation on the flow over a low-Re airfoil , 1987, Journal of Fluid Mechanics.
[11] L. Ericsson. Effect of Karman vortex shedding on airfoil stall flutter , 1986 .
[12] Thomas J. Mueller,et al. Low Reynolds Number Vehicles , 1985 .
[13] E. K. Armstrong,et al. Some Practical Aspects of Compressor Blade Vibration , 1960, The Journal of the Royal Aeronautical Society.
[14] W. Mccroskey,et al. Dynamic Stall Experiments on Oscillating Airfoils , 1975 .
[15] G. Cerri,et al. Experimental Analysis of the Wake Behind an Isolated Cambered Airfoil , 1981 .
[16] R. Simpson. Two-dimensional turbulent separated flow , 1987 .
[17] M. V. Dyke,et al. An Album of Fluid Motion , 1982 .
[18] F. Motallebi,et al. The effect of base bleed on vortex shedding and base pressure in compressible flow , 1981 .
[19] D. Rockwell. Oscillations of impinging shear layers , 1983 .
[20] K. Sreenivasan. Transitional and Turbulent Wakes and Chaotic Dynamical Systems , 1985 .
[21] Khairul Q. Zaman,et al. Natural large-scale structures in the axisymmetric mixing layer , 1984, Journal of Fluid Mechanics.
[22] D. J. Mckinzie,et al. A natural low frequency oscillation in the wake of an airfoil near stalling conditions , 1988 .
[23] Morteza Gharib,et al. Ordered and chaotic vortex streets behind circular cylinders at low Reynolds numbers , 1987, Journal of Fluid Mechanics.
[24] Andrew S. W. Thomas. The unsteady characteristics of laminar juncture flow , 1987 .
[25] Christopher L. Rumsey,et al. Upwind Navier-Stokes solutions for separated periodic flows , 1986 .
[26] R. L. Halfman,et al. Evaluation of high-angle attack aerodynamic-derivative data and stall-flutter prediction techniques , 1951 .
[27] W. K. Anderson,et al. Application of thin-layer Navier-Stokes equations near maximum lift , 1984 .
[28] Christopher L. Rumsey,et al. A computational analysis of flow separation over five different airfoil geometries at high angles-of-attack , 1987 .
[29] N. Moss. Measurements of aerofoil unsteady stall properties with acoustic flow control , 1979 .
[30] Valdis Kibens,et al. Discrete Noise Spectrum Generated by Acoustically Excited Jet , 1980 .
[31] Khairul Q. Zaman,et al. Far-field noise of a subsonic jet under controlled excitation , 1985, Journal of Fluid Mechanics.
[32] John E Baker. The effects of various parameters including Mach number on propeller blade flutter with emphasis on stall flutter , 1951 .
[33] R. H. Schlinker,et al. Progress in rotor broadband noise research , 1983 .