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    Modelling combustor performance of a ducted rocket

    Stowe, R. / De Champlain, A. / Mayer, A. | AIAA | 2000

    A new methodology for the analysis of experimental data describing pulse-triggered nonlinear instability in solid rocket motors

    Harris, P. / de Champlain, A. | AIAA | 1998

    Mixed convective heat transfer in an inclined cavity with multiple heated elements on one wall

    OOSTHUIZEN, P. / DE CHAMPLAIN, A. | AIAA | 1989

    Pulse-triggered nonlinear instability in solid rocket motors - An experimental study

    Harris, P. / de Champlain, A. / Bourque, C. | AIAA | 1997

    Direct fuel injection for bluff body flame stabilization

    Carrier, D. / De Champlain, A. / Bardon, M. | AIAA | 1996

    Two phase flow combustion modelling of a ducted rocket

    Stowe, R. / Dubois, C. / Harris, P. et al. | AIAA | 2001

    Supersonic PIV measurements in an open jet flow

    Hamel, N. / de Champlain, A. / Rainville, P.-A. et al. | AIAA | 2001

    Prediction of Soot Emissions in Gas Turbine Combustors

    De Champlain, A. / Kretschmer, D. / Tsogo, J. et al. | British Library Conference Proceedings | 1995

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