Studies on Pulse Jet Engine by Wind Tunnel Testing

Studies on Pulse Jet Engine by Wind Tunnel Testing

Simple design and efficiency make pulse jet engines attractive for aeronautical short-term operation applications. An active control system extends the operating range and reduces the fuel consumption considerably so that this old technology might gain a new interest. The results on wind tunnel expe...

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Veröffentlicht in:International Journal of Rotating Machinery 2001, Vol.2001 (2), p.79-85
Hauptverfasser: Nakano, Toshihiro, Zeutzius, Michael, Miyanishi, Hideo, Setoguchi, Toshiaki, Kaneko, Kenji
Format: Artikel
Sprache:eng
Schlagworte:
Active control
Compressible flow
Propulsion
Pulse combustion
Steady combustion
Wind tunnel testing
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Beschreibung
Zusammenfassung:Simple design and efficiency make pulse jet engines attractive for aeronautical short-term operation applications. An active control system extends the operating range and reduces the fuel consumption considerably so that this old technology might gain a new interest. The results on wind tunnel experiments have been reported together with the impact of combustion mode (pulse or steady) on system performance.
ISSN:1023-621X
1542-3034
1563-5090
DOI:10.1155/S1023621X01000070