1–20 von 81 Ergebnissen
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    Influence of Inlet Piping Conditions on Pump Performance in an Aircraft Engine Lubrication System

    Hendrick, P. / Ippoliti, L. | British Library Conference Proceedings | 2013

    Development and Testing of Advanced Surface Oil Coolers for Aero Engines

    Hendrick, P. / Outirba, B. | British Library Conference Proceedings | 2013

    Testing of Carbon Brush Seals for Aero-Engine Bearing Chambers

    Hendrick, P. / Outirba, B. | British Library Conference Proceedings | 2013

    Improved Performance Assessment of a Precooled Turbofan for Hypersonic Vehicle Acceleration

    Hendrick, P. / Verstraete, D. | British Library Conference Proceedings | 2011

    Hydrogen Fueled Precooled Airbreathing Engines for Hypersonic Aircraft and Spaceplanes

    Hendrick, P. / Verstraete, D. | British Library Conference Proceedings | 2011

    VPSC, a vehicle parametric sizing code

    Hendrick, P. | AIAA | 2001

    Design and Feasibility Study of a Turboshaft Equipped Two-Seat Kitcopter

    Buysschaert, F. / Hendrick, P. | British Library Conference Proceedings | 2007

    Experimental Study of an Air-Oil Pump and Separator Solution

    Hendrick, P. / Ippoliti, L. / Steimes, J. | British Library Conference Proceedings | 2013

    Hydrogen fuel tanks for subsonic transport aircraft

    Verstraete, D. / Hendrick, P. / Pilidis, P. et al. | Tema Archiv | 2010

    Mathematical Model of Brush Seal - A Nonlinear Analytical Solution

    Changizi, A. / Stiharu, I. / Hendrick, P. | British Library Conference Proceedings | 2011

    LOX collection - A highly synergistic technology

    Johnson, C. / Hendrick, P. | AIAA | 1999