1. A. H. Whitehead, Jr., ?Effect of vortices on delta-wing leeside heating at Mach 6,? AIAA J.,8, No. 3 (1970).
2. D. M. Rao and A. H. Whitehead, Jr., ?Leeside vortices on delta wings at hypersonic speeds,? AIAA J.,10, No. 11 (1972).
3. N. A. Davydova, Yu. I. Zaitsev, and A. Ya. Yushin, ?Experimental investigation of aerodynamic heating of the upper surface of flat triangular wings at supersonic speeds,? Uchen. Zap. Tsentr. Aerogidrod. Inst.,6, No. 5 (1974).
4. G. I. Maikapar, ?Aerodynamic heating of the leeward side of a body at supersonic speeds,? Uchen. Zap. Tsentr. Aerogidrod. Inst.,3, No. 6 (1972).
5. V. Ya. Borovoi, Gas Flow and Heat Transfer in Zones of Shock-Wave Boundary-Layer Interaction [in Russian], Mashinostroenie, Moscow (1983).