The Behaviour and Effects of Laminar Separation Bubbles on Aerofoils in Incompressible Flow
暂无分享,去创建一个
[1] T. W. F. Moore,et al. Some Experiments on the Reattachment of a Laminar Boundary Layer Separating From a Rearward Facing Step on a Flat Plate Aerofoil , 1960, The Journal of the Royal Aeronautical Society.
[2] P. R. Owen,et al. On the Laminar Boundary Layer Separation from the Leading Edge of a Thin Aerofoilv , 1953 .
[3] N. Curle,et al. Approximate Methods for Predicting Separation Properties of Laminar Boundary Layers , 1957 .
[4] L. F. Crabtree,et al. Prediction of Transition in the Boundary Layer on an Aerofoil , 1958, The Journal of the Royal Aeronautical Society.
[5] N. Tetervin. Investigation of the Variation of Lift Coefficient with Reynolds Number at a Moderate Angle of Attack on a Low-Drag Airfoil , 1942 .
[6] L. F. Crabtree,et al. Effects of Leading-Edge Separation on Thin Wings in Two-Dimensional Incompressible Flow , 1957 .
[7] Donald E. Gault,et al. Boundary-layer and stalling characteristics of the NACA 64A006 airfoil section , 1949 .
[8] L. W. Hunton,et al. An investigation at subsonic speeds of several modifications to the leading-edge region of the NACA 64A010 airfoil section designed to increase maximum lift , 1956 .
[9] Itiro Tani,et al. Critical survey of published theories on the mechanism of leading-edge stall. , 1961 .
[10] Von Doenhoff,et al. A preliminary investigation of boundary-layer transition along a flat plate with adverse pressure gradient , 1938 .
[11] Donald E. Gault,et al. Examples of three representative types of airfoil-section stall at low speed , 1951 .
[12] G. B. Schubauer,et al. Contributions on the Mechanics of Boundary-Layer Transition , 1955 .
[13] J. Black,et al. Some Measurements of Leading Edge Separation Bubbles on a 10 per cent Thick Symmetrical Aerofoil , 1953, The Journal of the Royal Aeronautical Society.
[14] R. Peterson. The Boundary-layer and Stalling Characteristics of the NACA 64A010 Airfoil Section , 1950 .
[15] D. Gault,et al. An Investigation at Low Speed of the Flow over a Simulated Flat Plate at Small Angles of Attack Using Pitot-static and Hot-wire Probes , 1957 .
[16] L. F. Crabtree,et al. SOME EFFECTS OF FLOW SEPARATIONS ON THIN WINGS WITH UNSWEPT LEADING EDGES , 1955 .
[17] D. Gault. A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry , 1957 .
[18] B. H. Lochtenberg. Transition in a Separated Laminar Boundary Layer , 1960 .
[19] G. B. Mccullough,et al. The effect of Reynolds number on the stalling characteristics and pressure distributions of four moderately thin airfoil sections , 1955 .
[20] T. W. Moore. A Note on the Causes of Thin Aerofoil Stall , 1959, The Journal of the Royal Aeronautical Society.