Detonation Jet Engine. Part 1--Thermodynamic Cycle

Autor/inn/en	Bulat, Pavel V.; Volkov, Konstantin N.
Titel	Detonation Jet Engine. Part 1--Thermodynamic Cycle
Quelle	In: International Journal of Environmental and Science Education, 11 (2016) 12, S.5009-5019 (11 Seiten) PDF als Volltext kostenfreie Datei Verfügbarkeit
Sprache	englisch
Dokumenttyp	gedruckt; online; Zeitschriftenaufsatz
ISSN	1306-3065
Schlagwörter	Thermodynamics; Efficiency; Engines; Physics; Scientific Research; Engineering; Air Transportation; Fuels; Comparative Analysis; Energy; Aviation Technology; Foreign Countries; Russia + Suchen Sie Ihr Suchwort? Thermodynamik; Effectiveness; Effektivität; Wirkungsgrad; Maschine; Physik; Maschinenbau; Treibstoff; Energie; Flugtechnik; Ausland; Russland
Abstract	We present the most relevant works on jet engine design that utilize thermodynamic cycle of detonative combustion. The efficiency advantages of thermodynamic detonative combustion cycle over Humphrey combustion cycle at constant volume and Brayton combustion cycle at constant pressure were demonstrated. An ideal Ficket-Jacobs detonation cycle, and the thermodynamic cycle of real detonation engine that utilizes over compressed detonation were discussed. Main trends in development of detonation engines were described. Relevant for nearest time problems and directions of research were formulated. (As Provided).
Anmerkungen	LOOK Academic Publishers. Knobbelzwaansingel 211 Den Haag 2496LN, Netherlands. Tel: 31-20-217-0912; e-mail: editor@lookacademy.nl; Web site: http://www.ijese.net
Erfasst von	ERIC (Education Resources Information Center), Washington, DC
Update	2020/1/01