1–20 von 66 Ergebnissen
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    Investigation of ionospheric irregularities and scintillation using TEC at high latitude

    Tiwari, R. / Strangeways, H.J. / Tiwari, S. et al. | Elsevier | 2013

    Drag reduction of a noncircular missile by base burning

    Ahmed, A. / Zumwalt, G. W. | AIAA | 1993

    On the juncture vortex in the transverse planes

    Khan, M. / Ahmed, A. | AIAA | 2002

    Development of the wake of an airfoil with riblets

    Caram, J.M. / Ahmed, A. | Tema Archiv | 1992

    Axisymmetric coaxial synthetic jets

    Bangash, Z. / Ahmed, A. | AIAA | 2002

    AIAA-2004-4732 Response of Vortex Breakdown Induced Wing Rock to Pitching & Plunging

    Khan, M. / Ahmed, A. | British Library Conference Proceedings | 2004

    StarLight - formation flying control architecture

    Ahmed, A. / Singh, G. | NTRS | 2002

    Scale and Condition Economies in Asset Preservation Cost Functions: Case Study Involving Flexible Pavement Treatments

    Irfan, M. / Khurshid, M.B. / Ahmed, A. et al. | British Library Online Contents | 2012

    Laser Doppler Velocimetry bias in wing-body juncture flow

    Khan, M.J. / Ahmed, A. | Tema Archiv | 1994

    Assessment of the Geomechanical Properties of Lunar Simulant Soils

    Newson, T. / Ahmed, A. / Joshi, D. et al. | TIBKAT | 2021

    Infant Pain Recognition with Homomorphic Filter and k-NN Classifier

    Mansor, M.N. / Junoh, A.K. / Ahmed, A. et al. | British Library Conference Proceedings | 2014

    Axisymmetric Jet Subjected to Radial and Azimuthal Forcing (AIAA 2014-2791)

    Ahmed, A. / Weiner, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    Mean Characteristics of Flow in Junctures of Swept Wings and Bodies

    Khan, M. J. / Ahmed, A. | British Library Online Contents | 1996

    Drag Reduction of the Space Shuttle

    Ahmed, A. / Khan, M. / AIAA | British Library Conference Proceedings | 1991

    Development of the wake of an airfoil with riblets

    Caram, J. M. / Ahmed, A. | NTRS | 1992