A novel hydrogen-fueled jet stabilized combustor for application in a hypersonic flight vehicle was investigated. Experimental and numerical investigations were carried out to arrive at the optimum design. Eight models were selected for combustion tests at air inlet temperature of 600 K. One of the selected models was also tested at elevated air inlet temperatures. It was found that the transverse fuel supply to the air jet was effective to get the highest combustion efficiency but it caused high pressure loss. The other alternative is to arrange the air injectors in tandem. It was found that when the mixture strength was close to the stoichiometric, the combustion efficiency deteriorated to 90 %.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Investigations of hydrogen-fueled turbo-ramjet engine combustors with jet stabilized flames


    Additional title:

    Untersuchungen von Brennkammern mit Flammen-Strahlstabilisierung für Wasserstoff als Treibstoff zum Einsatz in Turbinen-Staustrahltriebwerken


    Contributors:
    Tamaru, T. (author) / Shimodaira, K. (author) / Yamada, H. (author) / Kumar, S. (author) / Kinoshita, Y. (author) / Kitajima, J. (author)


    Publication date :

    1995


    Size :

    10 Seiten, 18 Bilder, 2 Tabellen, 7 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Investigations of Hydrogen-Fueled Turbo-Ramjet Combustors with Jet Stabilized Flames

    Tamaru, T. / Shimodaira, K. / Yamada, H. et al. | British Library Conference Proceedings | 1995


    Hydrogen-Fueled Jet-Stabilized Ramjet Engine Combustor Performance in Ramjet and Afterburning Combustion Modes

    Tamaru, T. / Shimodaira, K. / Kitajima, J. et al. | British Library Conference Proceedings | 1997


    Test Results of the Hydrogen Fueled Model Combustor for the Air Turbo Ramjet Engine

    Kashiwagi, T. / Obata, M. / Ohkita, Y. et al. | British Library Conference Proceedings | 1993


    Computer Modeling in Ramjet Combustors

    David G. Lilley | AIAA | 1981


    Design and Performance Analysis of Bio-Ethanol Fueled GG-Cycle Air Turbo Ramjet Engine

    Minato, Ryojiro / Higashino, Kazuyuki / Tanatsugu, Nobuhiro | AIAA | 2012