1. Owen, P. R. & Randall D. G. 1953 Boundary layer transition on a sweptback wing: a further investigation.RAE TM Aero 330.
2. Boltz F. W. , Kenyon, G. C. & Allen C. Q. 1960 Effects of sweep angle on the boundary layer stability characteristics of an untapered wing at low speeds.NASA TN D-338.
3. Owen, P. R. & Randall D. G. 1952 Boundary layer transition on a sweptback wing.RAE TM Aero 277.
4. Maltby, R. L. & Keating R. F. A. 1962 The surface oil flow technique for use in low speed wind tunnels.AGAR Dograph 70.
5. Anscombe, A. & Illingworth L. N. 1952 Wind-tunnel observations of boundary layer transition on a wing at various angles of sweep back. ARC R & M 2968.