Inflow-driven valve system for pulse detonation engines

Journal of Propulsion and Power

Volumn 27, Issue 3, 2011, Pages 597-607

  Matsuoka, Ken ^a   Yageta, Jun ^a   Nakamichi, Tatsuya ^a   Kasahara, Jiro ^a   Yajima, Takashi ^b   Kojima, Takayuki ^c  

^a UNIVERSITY OF TSUKUBA   (Japan)

^b IHI CORPORATION   (Japan)

^c JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; ENGINE PISTONS; ETHYLENE; FLOW RATE; JET ENGINES; MASS TRANSFER; OXYGEN SUPPLY; PISTONS; PULSE DETONATION ENGINES; ROCKETS;

INTERMITTENT FLOWS; MASS FLOW RATE MEASUREMENT; OPERATION FREQUENCY; PULSE DETONATION ROCKET ENGINES; SPECIFIC IMPULSE; STABLE OPERATION; SUPPLY PRESSURE; THRUST MEASUREMENT;

COMBUSTION KNOCK;

EID: 79955949405     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.47421     Document Type: Article

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