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    Transitional Shock Wave-Boundary Layer Interaction over a Cone Flare Model at Hypersonic Conditions

    Asma, C. / European Space Agency / CIRA et al. | British Library Conference Proceedings | 2002

    Orbital Dynamics Characteristics of a QB50 CubeSat Performing Atmospheric Reentry

    Asma, C. / Naviaux, J. / Kerschen, G. et al. | British Library Conference Proceedings | 2010

    Inducer-Induced Transition in Hypersonic Boundary Layers AIAA Paper

    Bottini, H. / Jivraj, F. / Strub, A. et al. | British Library Conference Proceedings | 2007

    Heatshield Qualification for the SpaceMail Re-Entry Capsule ``Fotino'' in the VKI Plasmatron

    Asma, C. / De Pascale, F. / Kruijff, M. et al. | British Library Conference Proceedings | 2008

    Footprint Analysis of the EXPERT Vehicle Winglet at Hypersonic Conditions

    Asma, C. / Van Der Haegen, V. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010

    Flow Topology of Gas, Liquid and 3-D Obstacles in Hypersonic Flow

    Asma, C. / Tirtey, S. / Schloegel, F. et al. | British Library Conference Proceedings | 2009

    Experimental Investigation of the Material Response of Carbon Composite Ablators in the VKI Plasmatron Facility

    Helber, B. / Asma, C. / Babou, Y. et al. | British Library Conference Proceedings | 2011

    Experimental Investigation of Liquid Fragmentation In Hypersonic Crossflow

    Asma, C. / Masutti, D. / Chazot, O. et al. | British Library Conference Proceedings | 2009

    Criteria Evaluation of 2-D Roughness Induced Transition for Expert Vehicle Design

    Masutti, D. / Chazot, O. / Asma, C. et al. | British Library Conference Proceedings | 2009