1. A. L. Gonor and N. A. Ostapenko, ?Hypersonic flow around a delta wing of finite thickness,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3 (1970).
2. B. A. Woods, ?Hypersonic flow with attached shock waves over delta wings,? Aeronaut. Quart.,21, No. 4 (1970).
3. J. Pike, ?The pressure on flat and anhedral delta wings with attached shock waves,? Aeronaut. Quart.,23, No. 4 (1972).
4. G. P. Vorkresenskii, ?Numerical solution of the problem of supersonic gas flow around an arbitrary delta wing surface in the compression domain,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4 (1968).
5. V. I. Lapygin and N. A. Ostapenko, ?Supersonic gas flow around the downwind side of a conical wing,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 1 (1973).