On the Effect of Internal Aerodynamics and Fuel Combustion Rate on the Thrust of a Valveless Pulsejet Engine

Author:

Migalin K. V.,Charntsev D. A.,Sidenko K. A.

Publisher

Allerton Press

Reference10 articles.

1. Pulse Jet Engine as the Future of the US Air Force: URL: https://vpk.name/news/521141_impulsnyi_reaktivnyi_dvigatel_kak_budushee_vvs_ssha.html.

2. Migalin, K.V. and Sidenko, K.A., Boosting the Combustion Process in an Ejector Bypass Pulsating Airbreathing Jet Engine, Izv. Vuz. Av. Tekhnika, 2022, vol. 65, no. 1, pp. 152–157 [Russian Aeronautics (Engl. Transl.), vol. 65, no. 1, pp. 173–179].

3. Migalin, K.V., Boichuk, I.P., and Sidenko, K.A., Inner Separation Area Precession as a Source for Initiating the Detonation or Quasi-Detonation Combustion in an Ejector Bypass Pulsejet Engine, Izv. Vuz. Av. Tekhnika, 2021, vol. 64, no. 3, pp. 113–118 [Russian Aeronautics (Engl. Transl.), vol. 64, no. 3, pp. 481–487].

4. Severyanin, V.S., Physics of Pulsating Combustion Devices, Vestnik Brestskogo Gosudarstvennogo Tekhnicheskogo Universiteta. Vodokhozyaistvennoe Stroitel’stvo, Teploenergetika i Geoekologiya, 2015, no. 2, pp, 43–46.

5. Ambrozhevich, A.V., Lar’kov, S.N., and Migalin, K.V., Technology of Numerical Research of the Working Processes of Transportation Systems with Valveless Pulsating Air-Jet Engines, Aviatsionno-Kosmicheskaya Tekhnika i Tekhnologiya, 2010, no. 4 (71), pp. 67–74.

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