1–5 of 5 hits
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    Acoustic vibration model of a composite shell with sound absorption material

    Dungan, M.R. / Mollo, C. / Vlahopoulos, N. et al. | Tema Archive | 1996
    only in two dimensions. This formulation assumes an isotropic structural member that couples with the elastic porous material. To expand beyond ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston
    Keywords: poröser Werkstoff , Scherung (Werkstoff)

    Fracture characterization of chopped-fiber glass composites /SMC/

    SUN, C. / SIERAKOWSKI, R. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Scanning Laser Doppler Vibrometry for the characterization of the damping loss factor in honeycomb panels

    Martarelli, Milena / Santolini, Claudio / Sassaroli, Andrea | Tema Archive | 2009
    experimental technique allows us to perform an accurate and high-spatial density measurement of the surface velocity of the structure. The two methods ...

    A comparison of optimization formulations for design minimization of aircraft interior noise

    Crane, S.P. / Cunefare, K.A. / Engelstad, S.P. et al. | Tema Archive | 1996
    were subject to upper and lower bounds on the design variables, the structural shell element thickness. All analyses were performed at a single ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Development of a pressure box to evaluate reusable-launch-vehicle cryogenic-tank panels

    Ambur, D.R. / Sikora, J. / Maguire, J.F. et al. | Tema Archive | 1996
    and frames can be adjusted to correspond to the tank structure by using these turnbuckles. The seal between the test panel and the cryogenic ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston