1–12 von 12 Ergebnissen
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    Short wide angle diffuser with pulse jet control

    Raghunathan, S. / Watterson, J. / Cooper, R. et al. | AIAA | 1999

    A novel concept of passive vortex generator jets

    Raghunathan, S. / Watterson, J. / Cooper, R. et al. | AIAA | 1999

    CFD investigation of excrescence effects on an engine nacelle external flow

    Humphries, P. / Kundu, A. / Cooper, R. et al. | AIAA | 1999

      CFD Investigation of Excrescence Effects on an Engine Nacelle External Flow

      Humphries, P. / Kundu, A. / Cooper, R. et al. | British Library Conference Proceedings | 1999

    AIAA-2004-6340 A Computational Investigation of Propulsion Integration

    Devine, R. / Crawford, B. / Benard, E. et al. | British Library Conference Proceedings | 2004

    Passive vortex control jets for shock boundary layer interactions

    Raghunathan, S. / O'Rourke, M. / Watterson, J. et al. | AIAA | 1999

    Performance and Acoustic Optimisation of Nacelle Nozzle Throat Area

    Sloan, B. / Wang, J. / Raghunathan, S. et al. | British Library Conference Proceedings | 2007

    Effect of Height and Density of Roughness Elements on Turbulent Boundary Layers

    Kerevanian, Grigorios-Kourken / Sidorenko, A. / Benard, E. et al. | AIAA | 2003

    Excrescence effects on boundary layers with pressure gradient at high subsonic speeds

    Raghunathan, S. / Riordan, D. / Humphries, P. et al. | AIAA | 2002

    THE AERODYNAMIC PERFORMANCE OF THE CASCADE WITHIN A THRUST REVERSER

    Yao, H. H. / Butterfield, J. / Raghunathan, S. et al. | British Library Conference Proceedings | 2004

    AIAA-2003-6748 Optimisation of a Thrust Reverser Cascade: An Assessment of Dynamic Response During Reverse Thrust

    Raghunathan, S. / Butterfield, J. / Yao, H. et al. | British Library Conference Proceedings | 2003

    Identification of aircraft noise at landing AIAA Paper 2005-2811

    Wang, J. / Yao, H. / Benard, E. et al. | British Library Conference Proceedings | 2005