1. Yuceil B, Dolling D S, Wilson D. A preliminary investigation of the helmholtz resonator concept for heat flux reduction. AIAA J, 1993, 2742
2. Yuceil, B, Dolling, D S. Effect of a nose cavity on heat transfer and flowfield over a blunt body at mach 5. AIAA J, 1994, 2050
3. Jiang Z L, Liu Y F, Han G L, et al. Experimental demonstration of a new concept of drag reduction and thermal protection for hypersonic vehicles. Acta Mech Sinica, 2009, 25: 417–419
4. Satheesh K, Jagadeesh G. Effect of concentrated energy deposition on the aerodynamic drag of a blunt body in hypersonic flow. Phys Fluids, 2007, 19: 1–4
5. Hayashi K, Aso S, Tani Y. Numerical study on aerodynamic heating reduction by opposing jet. Memoirs Faculty Eng Kyushu Univ, 2006, 66: 39–44