Search Results - "Zangiev, A. E."

Pulsed combustion of fuel–air mixture in a cavity above water surface: modeling and experiments by Frolov, S. M., Platonov, S. V., Avdeev, K. A., Aksenov, V. S., Ivanov, V. S., Zangiev, A. E., Sadykov, I. A., Tukhvatullina, R. R., Frolov, F. S., Shamshin, I. O.

“…A mathematical model for simulating combustion and detonation of a fuel–air mixture in the gas cavity above the free water surface is developed. The model is…”
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Pulsed combustion of fuel–air mixture in a cavity under the boat bottom: modeling and experiments by Frolov, S. M., Platonov, S. V., Avdeev, K. A., Aksenov, V. S., Ivanov, V. S., Zangiev, A. E., Sadykov, I. A., Tukhvatullina, R. R., Frolov, F. S., Shamshin, I. O.

“…The physical and mathematical model for simulating combustion and detonation of fuel mixture in the semi-confined gas volumes above the free surface of water…”
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Air-breathing pulsed detonation thrust module: Numerical simulations and firing tests by Frolov, S.M., Aksenov, V.S., Ivanov, V.S., Shamshin, I.O., Zangiev, A.E.

“…The air-breathing pulsed detonation thrust module (TM) for an aircraft designed for a subsonic flight at a speed of up to 120 m/s when operating on a standard…”
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Hydrogen fueled detonation ramjet: Conceptual design and test fires at Mach 1.5 and 2.0 by Ivanov, V.S., Frolov, S.M., Zangiev, A.E., Zvegintsev, V.I., Shamshin, I.O.

“…The conceptual design of a hydrogen-fueled detonation ramjet (DR) of a new type for a cruising flight speed of Mach 2 at sea level is developed using…”
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Updated conceptual design of hydrogen/ethylene fueled detonation ramjet: Test fires at Mach 1.5, 2.0, and 2.5 by Ivanov, V.S., Frolov, S.M., Zangiev, A.E., Zvegintsev, V.I., Shamshin, I.O.

“…The conceptual design of a hydrogen/ethylene fueled detonation ramjet (DR) studied earlier is updated based on numerical simulations and test fires at airflow…”
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Three-dimensional numerical simulation of the characteristics of a ramjet power plant with a continuous-detonation combustor in supersonic flight by Dubrovskii, A. V., Ivanov, V. S., Zangiev, A. E., Frolov, S. M.

“…Multi-variant three-dimensional numerical simulations demonstrate the feasibility of the continuous- detonation process in an annular combustor of a ramjet…”
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Thrust characteristics of an airbreathing pulse detonation engine in flight at mach numbers of 0.4 to 5.0 by Zangiev, A. E., Ivanov, V. S., Frolov, S. M.

“…Multidimensional calculations are performed to demonstrate that, by its characteristics, the pulse detonation engine (PDE) is a unique type of ramjet…”
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Chemiionization and acoustic diagnostics of the process in continuous- and pulse-detonation combustors by Frolov, S. M., Aksenov, V. S., Dubrovskii, A. V., Zangiev, A. E., Ivanov, V. S., Medvedev, S. N., Shamshin, I. O.

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3D versus 2D calculation of thrust characteristics of the air-breathing pulse detonation engine under supersonic flight conditions by Zangiev, A. E., Ivanov, V. S., Frolov, S. M.

“…3D calculations are used to confirm the conclusion that the specific thrust of the air-breathing pulse detonation engine is 20–30% higher than that of the…”
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Thrust characteristics of an airbreathing pulse detonation engine in supersonic flight at various altitudes by Zangiev, A. E., Ivanov, V. S., Frolov, S. M.

“…The main thrust characteristics, such as thrust force, specific impulse, specific fuel consumption, and specific thrust, of a pulse detonation engine (PDE)…”
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