1. GAULT, D. E., An Investigation at Low Speed of the Flow over a Simulated Flat Plate at Small Angles of attack Using Pitotstatic and Hot-wire Probes. NACA TN 3876, March 1957
2. Types of Flow on Swept Wings with Special Reference to Free Boundaries and Vortex Sheets;KUCHEMANN;J. Roy. Aero. Soc,1953
3. WALLIS, R. A., Experiments with Air Jets to Control the Nose Stall on a 3 ft Chord NACA 64A006 Aerofoil, A.R.L. Aero. Note 139, Sept. 1954
4. WALLIS, R. A. and RUGLEN, N., A., Note on the Cause of the Nose Stall of Thin Wings, A.R.L. Aero. Note. 161, May 1957
5. The Structure of the Turbulent Boundary Layer;TOWNSEND;Proc. Camb. Phil. Soc,1951