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    On the energy efficiency of hydrogen-fuelled transport aircraft

    Verstraete, D. | Tema Archive | 2015

    MULTI-DISCIPLINARY OPTIMISATION OF MEDIUM ALTITUDE LONG ENDURANCE UAVS

    Verstraete, D. | British Library Conference Proceedings | 2018

    Characterisation of a hybrid, fuel-cell-based propulsion system for small unmanned aircraft

    Verstraete, D. | Online Contents | 2014

    Demonstration of Compact Air Separation Technology for In-Flight Oxygen Collection Space Launchers

    Verstraete, D | Online Contents | 2014

    Impact of Heat Transfer on the Performance of Micro Gas Turbines

    Verstraete, D. | British Library Conference Proceedings | 2013

    PROPELLER OPTIMISATION FOR AN ELECTRICAL-POWERED TACTICAL UAS

    Macneill, R. / Verstraete, D. | British Library Conference Proceedings | 2018

    Development of a Semi-Constant Volume Combustor for a Micro Gas Turbine

    Armstrong, J. / Verstraete, D. | British Library Conference Proceedings | 2013

    LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE

    Bykerk, T. / Pezzella, G. / Verstraete, D. | British Library Conference Proceedings | 2021

    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

    FLIGHT TEST OF A FUEL-CELL/BATTERY/SUPERCAPACITOR TRIPLE HYBRID UAV PROPULSION SYSTEM

    Gong, A. / Palmer, J. L. / Verstraete, D. | British Library Conference Proceedings | 2018

    Hydrogen fuel tanks for subsonic transport aircraft

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

    Analysis of the Performance of Fuel-Cell-Based Hybrid-Electrical UAS Propulsion Through Hardware-in-the-Loop Simulation

    Harvey, J.R. / Palmer, J.L. / Verstraete, D. | British Library Conference Proceedings | 2013

    MULTI-OBJECTIVE OPTIMISATION OF SEMI-CLOSED CYCLE ENGINES FOR HIGH ALTITUDE UAV PROPULSION

    Tacconi, J. / Visser, W. P. J. / Verstraete, D. | TIBKAT | 2021

    Comparison of Propulsion Technologies for a HALE Airship

    Hendrick, P. / Hallet, L. / Verstraete, D. | British Library Conference Proceedings | 2007

    Characterisation of a hybrid, fuel-cell-based propulsion system for small unmanned aircraft

    Verstraete, D. / Lehmkuehler, K. / Gong, A. et al. | Tema Archive | 2014

    Development of a Micro Turboprop for High Altitude UAV Propulsion

    Armfield, S. / Ling, J. / Verstraete, D. et al. | British Library Conference Proceedings | 2011

    Experimental Characterization of a Fuel Cell Hybrid Electrical UAV Propulsion System (AIAA 2014-0017)

    Gong, A. / Verstraete, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    STRUCTURAL DESIGN OPTIMISATION AND AEROTHERMOELASTIC ANALYSIS OF LAPCAT A2 MACH 5 CRUISE VEHICLE (AIAA 2014-2294)

    Sharifzadeh, S. / Hendrick, P. / D Mello, S. et al. | British Library Conference Proceedings | 2014

    HYDROGEN FUELLED LARGE LONG RANGE TRANSPORT AIRCRAFT

    Verstraete, D. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2006

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