References
- Godunov, S.K. 1959. A difference method for numerical calculation of discontinuous solutions of Hydrodynamics. Math. Collection., 47(89), No 3, 271.
- Harten, A. 1983. High resolution schemes for hyperbolic conservation laws. J. Computation.Physics., 49, 357.
- Levin, V.A., Nechaev, J.N., and Tarasov, A.I. 2001. A new approach to organizing operation cycles in pulsed detonation engines. In Roy, G., Frolov, S., Netzer, R., and Borisov, A. (Eds.) High-Speed Deflagration and Detonation: Fundamentals and Control. TORUS PRESS: Moscow, pp. 223–238.
- Levin, V.A., Perezhogin, V.N., and Khmelevsky, A.N. 1995. Feature of combustion products flow structure in spherical semi-open cavity. Combust, Explosion and Shock 1995., 31(1), 30–36.
- Levin, V.A., Afonina, N.E., Gromov, V.G., Smekhov, G.D., Khmelevsky, A.N., and Markov, V.V. 2010. Dynamic of combustion products flow in ring nozzle with a half-closed cavity. Combust. Sci. Technol., 182(11–12), 1–16.
- Levin, V.A., Afonina, N.E., Gromov, V.G., Smekhov, G.D., Khmelevskii, A.N., and Markov, V.V. 2012. Gas dynamics and thrust in the exhaust system of a jet engine with an annular nozzle. Combustion, Explosion and Shock Waves., 48(4), 406–417.
- Levin, V.A., Afonina, N.E., Gromov, V.G., Manuylovich, I.S., Markov, V.V., Smekhov, G.D., and Khmelevskii A.N. 2013. Experimental and numerical simulation of the flow in a driving module with an annular and linear double-slot nozzle. High Temp, 51(5), 681–689.
- Levin, V.A., Afonina, N.E., Gromov, V.G., Smekhov, G.D., Khmelevskii, A.N., and Markov, V.V. 2013. Investigating an annual nozzle on combustion products of hydrocarbon fuels. Thermophysics and Aeromechanic, 20(3), 263–269.
- Levin, V.A., Afonina, N.E., Gromov, V.G., Manuylovich, I.S., Markov, V.V., Smekhov G.D., and Khmelevskii, A.N. 2015. Pulsating gas flows in an annular nozzle. Doklady Physics. 60(11), 500–503.
- Levin, V.A., Afonina, N.E., Gromov, V.G., Manuylovich, I.S., Markov, V.V., Smekhov G.D., and Khmelevskii, A.N. 2016. Unsteady Laminar Gas Flows in an Annular Nozzle. High Temp, 54(6), 837–841.
- Leyva, I.A., Tangirala, V.E., and Dean, A.J. 2003. Investigation of unsteady flow field in a 2-Stage PDE resonator: AIAA Paper № 2003–0715 (41st Aerospace Sciences Meeting & Exhibit, 6-9 January, Reno, Nevada, 10 pp).
- Marchukov, E.Yu., Tarasov, A.I., and Wagner A.V. 2006. Testing results of valve less pulse engine demonstrator and numerical simulation. In Roy, G., and Frolov, S. (Eds) Pulse and Continuous Detonation Propulsion. TORUS PRESS: Moscow, pp. 294–298.
- McManus, K.R., and Dean, A.J. 2005. Experimental evaluation of a two stage pulse detonation combustor. AIAA Paper № 2005-3773, (41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 10 13 July, 2005, Tucson, Arizona, 8 pp).
- Nechaev, Yu.N., Polev, A.S., and Tarasov, A.I. 2002. Results of an experimental study of kerosene-air pulse detonation engines and problems associated with their practical implementation. In Roy, G.D., Frolov, S.M., Santoro, R.J. Tsyganov, S.A. (Eds) Advances in confined detonations. TORUS PRESS: Moscow, pp. 221–224.
- Taki, S., and Fujiwara, T. 2004. A numerical study of detonation resonator. In Roy, G., Frolov, S., and Shepherd J. (Eds.). Application of Detonation to Propulsion. TORUS PRESS: Moscow, pp. 257–261.
- Taki, S., and Fujiwara, T. 2006. A numerical study of detonation resonator. In Roy, G., and Frolov, S. (Eds.) Pulse and Continuous Detonation Propulsion. TORUS PRESS: Moscow, pp. 309–320.
- Zeng, H., He, L.-M., and Chen., W. 2015. Investigation on shock wave focusing in 2-Stage PDE. Papers of 25th International Colloquium on the Dynamics of Explosions and Reactive Systems, 2-7 August, Leeds, UK, No. 309.