1. Lighthill, M. J., “On Boundary Layers and Upstream Influence; II, Supersonic Flow Wighout Separation,” Proc. Royal Soc, A217, No. 1131, pp. 478–507, 1953.
2. Mason, W. H. and G. R. Inger, “Analytical Study of Transonic Normal Shock-Boundary Layer Interaction,” VPI & SU Report Aero-027, Blacksburg, Va., November 1974. AIAA Paper 75-831, June 1975.
3. Adams, M. C., “On Shock Waves in Inhomogeneous Flow,” JAS, Vol. 16, No. 9, pp. 590–685, September 1949.
4. Inger, G. R., “Compressible Boundary Layer Flow Past a Swept Wavy Wall with Heat Transfer and Ablation,” Astronautica Acta 19, pp. 325–338, 1971.
5. Ackeret, J., Feldman, F., and Rott, N., “Investigation of Compression Shocks and Boundary Layers in Gases Moving at High Speeds,” NACA TM 1113, 1947.