1. Van Dyke M.D. Second-order slender-body theory − axisymmetric flow // NASA Tech. Rep. 1959. R-47. 26 p.
2. Cole J.D. Perturbation methods in applied mathematics. Waltham: Blaisdell, 1968. 260 p.
3. Jones R.T. Leading-edge singularities in thin-airfoil theory // J. Aeronaut. Sci. 1950. V. 17. № 5. P. 307−310.
4. Van Dyke M.D. Second-order subsonic airfoil theory including edge effects // NACA Rep. 1956. № 1274. 23 p.
5. Van Dyke M. Perturbation methods in fluid mechanics. Stanford: Parabolic Press, 1975. 271 p.