1–10 von 10 Ergebnissen
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    AIAA 2001 - 0130 "Channel" & "Arc" Wing Aerodynamics With Propeller Effects for STOL Application

    Nangia, R. K. / Palmer, M. E. / AIAA | British Library Conference Proceedings | 2001

    Negatively Scarfed Inlets for Acoustic Reduction, Aerodynamic Performance Assessment

    Nangia, R. K. / Palmer, M. E. / AIAA | British Library Conference Proceedings | 2000

    Flow Separation Prediction on Inlets with Mach and Reynolds Number Effects in Subsonic Flight

    Nangia, R. K. / Palmer, M. E. / Hodges, J. | British Library Online Contents | 1996

    UNCONVENTIONAL HIGH ASPECT RATIO JOINED-WING AIRCRAFT WITH AFT- & FORWARD- SWEPT WING-TIPS

    Nangia, R. K. / Palmer, M. E. / Tilmann, C. P. et al. | British Library Conference Proceedings | 2003

    AIAA 2006-0859 Joined Wing Configuration for High Speeds - A First Stage Aerodynamic Study

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

    Modelling of 3D Aircraft Inlets at "Zero" Speed (and Low Speeds with Cross-Wind) and Flow Separation Prediction

    Nangia, R. K. / Palmer, M. E. / Hodges, J. et al. | British Library Conference Proceedings | 1998

    Planform Variation Effects in Unconventional High Aspect Ratio Joined-Wing Aircraft Incorporating Laminar Flow

    Nangia, R. K. / Palmer, M. E. / Tilmann, C. P. et al. | British Library Conference Proceedings | 2005

    DESIGN OF HIGH ASPECT RATIO "LAMBDA-WINGS" INCORPORATING LAMINAR FLOW

    Nangia, R. K. / Palmer, M. E. / Tilmann, C. P. et al. | British Library Conference Proceedings | 2004

    Towards Design of a Novel High Altitude Joined-Wing Sensor-Craft

    Nangia, R. K. / Palmer, M. E. / Tilmann, C. P. et al. | British Library Conference Proceedings | 2004

    Flow Separation Prediction on Inlets with Mach and Reynolds Number Effects in Subsonic Flight

    Nangia, R. K. / Palmer, M. E. / Hodges, J. et al. | British Library Conference Proceedings | 1996