1. Mangler, K. W., Smith, J. H.: Calculation of the flow past slender delta wings with leading edge separation. RAE Report Aero 2593, May 1957.
2. Stewartson, K., Hall, M. G.: The inner viscous solution for the core of a leading edge vortex. Journ. of Fluid Mechanics13, 306?318 (1963).
3. Legendré, R.: Flow in the neighbourhood of the apex of a highly swept wing at moderate incidence. La recherche Aeronautique, no. 30, 1952, Vols. 31 and 35, 1953 (translated by Sylvia W. Skan of the Aerodynamics division, National Physical Laboratory).
4. Adams, M. C.: Leading edge separations from delta wings at supersonic speeds. Journ. of Aero. Sciences (Reader's forum)1953, 430.
5. Smith, J. H. B.: Improved calculations of leading edge separation from slender delta wings. RAE Tech. report no: 66070, March, 1966.