1–14 von 14 Ergebnissen
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    Heat Transfer to a Swept Leading Edge in Hypersonic Flow Including Effects of Surface Transpiration

    Poll, D. I. A. / IUTAM | British Library Conference Proceedings | 1994

    Experimental and computational investigation of leading edge transition at Mach 1.6

    Coleman, Colin / Poll, D. / Line, Ray-Sing | AIAA | 1997

    Natural and Hybrid Laminar Flow Control for Aero-Engine Nacelles

    Mullender, A. J. / Poll, D. I. A. | SAE Technical Papers | 1995

    Leading edge transition on a 76 degree swept cylinder at Mach 1.6

    Coleman, Colin / Laub, James / Poll, D. et al. | AIAA | 1996

    Reynolds number effects on the flow around 2-D ellipses at incidence

    Lamont, P / Poll, D / Taghavi-Zenouz, R | AIAA | 1995

    Hybrid Laminar Flow Technology for Aero-Engine Nacelles

    Mullender, A. J. / Poll, D. I. A. / International Society for Air Breathing Engines; Australian Committee | British Library Conference Proceedings | 1995

    Aircraft Drag Reduction: The Application of Natural Laminar Flow to Aero-Engine Nacelles

    Mullender, A. J. / Poll, D. I. A. / International Society for Air Breathing Engines; Australian Committee | British Library Conference Proceedings | 1995

    Hypersonic Laminar-Turbulent Transition and its Implications for Winged Configurations

    Poll, D. I. A. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research &Development; Fluid Dynamics Panal | British Library Conference Proceedings | 1996

    Assessment of the e^N Method as a Transition Prediction Tool for Zero Pressure Gradient Flows with and without Boundery Layer Suction

    Ellis, J. E. / Walsh, S. A. / Poll, D. I. A. et al. | British Library Conference Proceedings | 2001

    Implications of 3-D transition mechanisms on the performances of space vehicles

    Poll, D. I. A. / European Space Agency / Institut national de recherche en informatique et en automatique et al. | British Library Conference Proceedings | 1995