1–20 of 207 hits
|

    Fatigue crack growth in diffusion bonded stiffened skin structure

    KATCHER, M. | AIAA | 1974
    Publisher: The American Institute of Aeronautics and Astronautics

    Analysis of thick rectangular plates laminated of bimodulus composite materials

    BERT, C. / REDDY, J. / REDDY, V. et al. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Honeycomb sandwich joints for primary structure

    SOUDAK, U. / HAMM, R. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Fatigue and fracture behavior of the high hardenability martensitic 'Transage' titanium alloys

    CROSSLEY, F. / JEAL, R. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Boundary-layer hygroscopic stresses in angle-ply composite laminates

    WANG, S. / CHOI, I. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    The influence of hole quality on graphite epoxy composite laminates

    PENGRA, J. / WOOD, R. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Elastic stability of superplastically formed/diffusion-bonded orthogonally corrugated core sandwich plates

    KO, W. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Failure stress correlation of composite laminates containing a crack

    CHU, C. / FREYRE, O. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Compression fatigue analysis of fiber composites

    RATWANI, M. / KAN, H. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Stress analysis of holes in angle-ply laminates - An efficient assumed stress 'special-hole-element' approach

    NISHIOKA, T. / ATLURI, S. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Built-up low-cost advanced titanium structures /BLATS/

    FRANKLIN, W. / WAITZ, C. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Fracture characterization of chopped-fiber glass composites /SMC/

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

    The effects of compression-compression fatigue on balanced graphite/epoxy laminates with holes

    MAR, J. / GRAVES, M. / MAASS, D. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Revision of maximum stress criterion of combined modes of fracture

    WANG, T. / TU, S.-Y. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Fatigue sensitivity of composite structure for fighter aircraft

    JEANS, L. / GRIMES, G. / KAN, H. | AIAA | 1981
    Publisher: The American Institute of Aeronautics and Astronautics

    A building block approach to design verification testing of primary composite structure

    WHITEHEAD, R. / DEO, R. | AIAA | 1983
    Publisher: The American Institute of Aeronautics and Astronautics

    Crash energy absorbing composite sub-floor structure

    FARLEY, G. | AIAA | 1986
    Publisher: The American Institute of Aeronautics and Astronautics

    Ingot metallurgy aluminum - Lithium alloys for aircraft structure

    EKVALL, J. / CHELLMAN, D. | AIAA | 1986
    Publisher: The American Institute of Aeronautics and Astronautics

    Designing Space Station structure for assembly

    RIEL, F. | AIAA | 1988
    Publisher: The American Institute of Aeronautics and Astronautics

    Durability prediction of complex panels with fluid-structure interaction

    FERMAN, M. / HEALEY, M. / RICHARDSON, M. | AIAA | 1988
    Publisher: The American Institute of Aeronautics and Astronautics