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    High thermal conductivity graphite in space applications

    Peck, S.O. | Tema Archive | 1995
    Applications of high thermal conductivity graphite fibers to space structures are discussed in the context of a composite scan mirror and ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Modeling of shock propagation and attenuation in viscoelastic materials

    Rusovici, R. / Lesieutre, G.A. / Inman, D.J. | Tema Archive | 2000
    address modeling of geometrically complex structures. These finite elements are then used to model shock propagation and absorption through ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Propagation and control of crack-like damage in curved composite panels under combined loads

    Mahler, M. / Ley, R. / Shah, C. et al. | Tema Archive | 2000
    Certification and damage tolerance criteria are critical technologies for the advancement of composites structures on commercial aircraft ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Damage tolerance of fiber composite airfoils with piezoelectric adaptive control system

    Minnetyan, L. / Chamis, C.C. / Abdi, F. | Tema Archive | 2000
    . Progressive damage and fracture of a laminated composite airfoil subjected to external pressure loading and adaptive control stresses is evaluated via ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Inclusions in Ti-6Al-4V investment castings

    Cotton, J.D. / Clark, L.P. / Reinhart, T.R. et al. | Tema Archive | 2000
    This paper some technical issues with Ti6Al4V airframe investment castings during the engineering and manufacturing development phase of ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Stiffness tailoring of tension loaded composite panels to contain crack-like damage

    Ley, R. / Lin, Weichuan / Mahler, M. et al. | Tema Archive | 2000
    change, an analytical methodology was developed based on separate examination of shear and normal strain failure indices at the damage tip ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Corrosion prediction in aging aircraft materials using neural networks

    Bailey, R.A. / Pidaparti, R.M. / Jayanti, S. et al. | Tema Archive | 2000
    exposed to two corrosive environments. Given the corrosion environment and time of exposure the first neural network predicts the ASTM G34 ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Predicting the impact response of an energy-absorbing composite subfloor beam

    Knight, N.F. jun. / Kellas, S. / Pinson, L.D. | Tema Archive | 2000
    applications. The paper presents an overview of the background design information for energy-absorbing composite subfloor beams and defines a specific ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Damage tolerance of cracked cylindrical shells under internal pressure

    Hoogkamer, D. / Waas, A.M. / Arbocz, J. | Tema Archive | 2000
    centralized cracks at angles to the shell generators ranging from 0 degree to 90 degree at an interval of 15 degree and of various crack length, are ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Durability of a woven polymer matrix composite in aerospace applications

    Patel, S.R. / Case, S.W. | Tema Archive | 2000
    The objective of this effort was to evaluate and model the effects of moisture, temperature, and combined hygrothermal aging on the ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

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