Drag reduction by controlled base flow separation for missile shaped bodies flying at hypersonic Mach number

Menezes, V., Sun, M., Jagadeesh, G., Reddy, K. P. J., & Takayama, K. (2005). Drag reduction by controlled base flow separation for missile shaped bodies flying at hypersonic Mach number. In Shock Waves (pp. 119–124). Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-27009-6_14