1. N. Frink, D. Bonhaus, V. Vatsa, et al., “A boundary condition for simulation of flow over porous surfaces,” in: Proc. of the 19th Applied Aerodynamics Conf. (Anaheim, June 11–14, 2001), AIAA, Hampton (2001), pp. 2001–2412.
2. T. Hartman and J. M. Morgenstern, “Passive aerodynamic sonic boom suppression for supersonic aircraft,” USA Patent No. 2004/0065774 A1 USA, Publ. 04.08.04.
3. V. N. Zaikovskii, V. P. Kiselev, S. P. Kiselev, et al., “Effect of a porous insert in the supersonic part of the nozzle in changes in the nozzle thrust,” Dokl. Ross. Akad. Nauk, 401, No. 4, 479–482 (2005).
4. N. I. Sidnyaev, “Review of methods for studying hypersonic gas flows past bodies with ablative coatings,” Thermophys. Aeromech., 11, No. 4, 489–508 (2004).
5. A. I. Shvets and I. T. Shvets, Near-Wake Gas Dynamics [in Russian], Naukova Dumka, Kiev (1976).