1–20 von 42 Ergebnissen
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    Adaptive Nonlinear Control of Multiple Spacecraft Formation Flying

    Marcio S. De Queiroz / Vikram Kapila / Qiguo Yan | AIAA | 2000

    Aerodynamic characteristics for a slender missile with wrap-around fins

    CATANI, U. / DE AMICIS / R. et al. | AIAA | 1983

    A forecast of air travel and airport and airway use in 1980

    De Vany, Arthur S. / Garges, Eleanor H. | Elsevier | 1971

    An empirical model of the F1 intermediate layer true-height characteristics

    González, M.Mosert de / Radicella, S. | Elsevier | 1987

    Artificial Dissipation Schemes for Viscous Airfoil Computations

    K. Frew / D. W. Zingg / S. De Rango | AIAA | 1998

    Assessment of a General Aviation Pilot Assisting System Influence on the Piloting Performance and Safety of Inexperienced Pilots

    Santana, Guilherme A. / de Oliveira, Paulo H. Iscold A. / Cimini, Carlos A. | Trans Tech Publications | 2014
    Beteiligte: de Oliveira, Paulo H. Iscold A. , Ferreira, Leonardo De Paula S.

    Buckling of Composite Plates with Local Damage and Thermal Residual Stresses

    Sé, rgio Frascino M-uacute / ller de Almeida / Jorn S. Hansen | AIAA | 2002

    Calculation of particle trajectories in solid-rocket motors with arbitrary acceleration

    SABNIS, JAYANT S. / DE JONG / FREDERICK J. et al. | AIAA | 1992

    Calculation of the two-phase aft-dome flowfield in solid rocket motors

    MADABHUSHI, RAVI K. / SABNIS, JAYANT S. / DE JONG et al. | AIAA | 1991

    Design and Evaluation of a Haptic Flight Director

    S. de Stigter / M. Mulder / M. M. Van Paassen | AIAA | 2007

    Full Validation of the StructuralAcoustic Response of a Simple Enclosure

    S. De Rosa / F. Franco / F. Marulo et al. | AIAA | 1999

    Generalization of Foreshortening Through New Reduced Geometrically Nonlinear Structural Formulation

    Javier Urruzola / Juan Tom-Uuml / s Celig-uacute et al. | AIAA | 2000