1–20 von 34 Ergebnissen
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    A "Tolerant" Wing Design for UCAV

    Nangia, R / Palmer, M. | AIAA | 2011

      A ``TOLERANT'' WING DESIGN FOR UCAV

      Nangia, R. / Palmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    Decentralise NHS data

    Palmer, M. | British Library Online Contents | 2004

    In the driver seat: The problems of vehicle leasing

    Palmer, M. | British Library Online Contents | 1996

    A study of supersonic aircraft with thin wings of low sweep

    Nangia, R. / Palmer, M. / Doe, R. | AIAA | 2002

    AIAA-2003-5452 A High-Performance Simulated On-Board Avionics Architecture to Support Traffic Operations Research

    Palmer, M. / Ballin, M. / AIAA | British Library Conference Proceedings | 2003

    AIAA-2004-5071 Towards Desgn of Long-Range Supersonic Military Aircraft

    Nangia, R. / Palmer, M. / Iwanski, K. | British Library Conference Proceedings | 2004

    AIAA-2004-5070 Towards Design of Mach 1.6+ Supersonic Cruise Aircraft

    Nangia, R. / Palmer, M. / Doe, R. | British Library Conference Proceedings | 2004

    AIAA-2003-6725 Airborne Conflict Resolution for Flow-Restricted Transition Airspace

    Mondoloni, S. / Palmer, M. / Ballin, M. et al. | British Library Conference Proceedings | 2003

    AIAA-2002-4446 Development of a Prototype Airborne Conflict Detection and Resolution Simulation Capability

    Mondoloni, S. / Palmer, M. / Wing, D. et al. | British Library Conference Proceedings | 2002

    AIAA-2004-1916 Dynamic Analysis and Parameter Optimization of a Fiber Optic Sensor Using Neural Networks

    Kim, Y. / Kapania, R. / Johnson, E. et al. | British Library Conference Proceedings | 2004

    Formation Flying Commercial Aircraft - Assessment Using a New Approach - Wing Span Load and Camber Control AIAA Paper

    Nangia, R. / Palmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    Formation Flying of Oblique Wing Aircraft, Assessment of Variations in Formation Configuration - Induced Effects & Control

    Nangia, R. / Palmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    Leading Edge Vortex Flaps on Moderate Sweep Wings- UCAV, Flow Improvement at High Lift AIAA Paper

    Nangia, R. / Palmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    Formation Flying of Commercial Aircraft, Variations in Relative Size/Spacing - Induced Effects & Control Induced Effects & Control

    Nangia, R. / Palmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    Morphing UCAV Wings Incorporating In-plane & Folding Tips - aerodynamic Design Studies

    Nangia, R. / Palmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006