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

    Poll, D. I. A. | British Library Online Contents | 1995

    Laminar-Turbulent Transition

    Poll, D. I. A. | British Library Online Contents | 1996

    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

    Surface suction on aerofoil aerodynamic characteristics at transonic speeds

    Qin, N / Zhu, Y / Poll, D I A | SAGE Publications | 1998

    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

    Visualization of non-equilibrium dissociating flows

    Han, J H / Kennaugh, A / Poll, D I A | SAGE Publications | 1997

    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