1–20 von 32 Ergebnissen
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    Whither reliabilityques

    DE S. COUTINHO / J. | AIAA | 1965

    Adaptive Nonlinear Control of Multiple Spacecraft Formation Flying

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

    Design and Evaluation of a Haptic Flight Director

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

    Shock Reflection Detonation Initiation Studies for Pulse Detonation Engines

    B. de Witt / G. Ciccarelli / F. Zhang et al. | AIAA | 2005

    Variations of Acoustic and Diffuse Mismatch Models in Predicting Thermal-Boundary Resistance

    Lisa De Bellis / Patrick E. Phelan / Ravi S. Prasher | AIAA | 2000

    Tail Buffet Alleviation of High-Performance Twin-Tail Aircraft Using Piezostack Actuators

    S. Hanagud / M. Bayon de Noyer / H. Luo et al. | AIAA | 2002

    Sandwich-Plate Vibration Analysis: Three-Layer Quasi-Three-Dimensional Finite Element Model

    Airton Nabarrete / Sergio Frascino M. De Almeida / Jorn S. Hansen | AIAA | 2003

    Artificial Dissipation Schemes for Viscous Airfoil Computations

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

    Quaternion-Based Adaptive Attitude Tracking Controller Without Velocity Measurements

    B. T. Costic / D. M. Dawson / M. S. de Queiroz et al. | AIAA | 2001

    Buckling of Composite Plates with Local Damage and Thermal Residual Stresses

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

    Structural acoustic calculations in the low-frequency range

    De Rosa / S. / Pezzullo, G. et al. | AIAA | 1994

    Aerodynamic characteristics for a slender missile with wrap-around fins

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

    Hybrid Navier-Stokes/Monte Carlo method for reacting flow calculations

    DE JONG / FREDERIK J. / SABNIS, JAYANT S. 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