21 research outputs found

    Unsteady aerodynamics and aeroelastic research at AFWAL

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    An efficient and accurate transonic unsteady aerodynamic method is needed for predicting flight loads, flutter and aeroelastic stability for advanced aircraft. There have been new developments and many improvements to older codes. XTRAN3S was improved and is a useful code for the near term. However, to predict the unsteady aerodynamics for high performance maneuvering aircraft, the Euler/Navier-Stokes codes must be extended and improved for complex 3-D configurations. The long term goal is development of Euler/Navier-Stokes unsteady aerodynamic methods for aeroelastic analysis

    Study of Dynamic Voltage Stability of Power Systems

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    Dr H. Thulié. — Le dressage des jeunes dégénérés. — Paris, F. Alcan, 1900

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    Philippe Jean. Dr H. Thulié. — Le dressage des jeunes dégénérés. — Paris, F. Alcan, 1900. In: Revue internationale de l'enseignement, tome 42, Juillet-Décembre 1901. pp. 465-466

    PAN AIR Applications to Weapons Carriage and Separation

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