51–57 of 57 hits
|

    Genetic algorithmus in multidisciplinary rotor blade design

    Hajela, P. / Lee, J. | Tema Archive | 1995
    efficiency, and a natural approach to account for the coupling between temporarily decoupled sub-problems. The design space for this problem is ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Health monitoring of reusable composite cryogenic tanks

    Emery, L. / Zisk, E.J. | Tema Archive | 1995
    Martin Marietta Manned Space Systems is developing methodologies to automatically and efficiently determine the health of reusable ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    An enhanced analysis method for composite overwrapped pressure vessels

    Shu, J.C. / Chiu, S.T. / Chang, J.B. | Tema Archive | 1995
    The increasing use of composite overwrapped pressure vessels (COPVs) in space applications demands a comprehensive and reliable analysis ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Unsteady aerodynamics of a flapped airfoil in subsonic flow by indicial concepts

    Hariharan, N. / Leishman, J.G. | Tema Archive | 1995
    An approach, based on the indicial method, is described for computing the unsteady lift, pitching moment, hinge moment and the drag on a ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Prediction of acoustically induced random vibration loads for shuttle payloads

    Leung, K. / Foist, B.L. | Tema Archive | 1995
    This paper presents a method for predicting random vibration loads for National Space Transportation System (NSTS) Shuttle launched ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Development of a low cost all composite satellite bus primary structure

    Braun, B. / Davinic, N. / Simon, W. | Tema Archive | 1995
    composite spacecraft bus, the Naval Center For Space Technology (NCST) at the Naval Research Laboratory (NRL), has designed and built a light weight ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    A physical explanation of free play effects on the flutter response of an all movable control surface

    Pitt, D.M. | Tema Archive | 1995
    Aicraft Modeling Using State Space', (FAMUSS), computer code was used to generate state models at selected velocities. Two different state models ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington