1–20 of 1,433 hits
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    DIFFUSION BONDING OF TITANIUM SANDWICH STRUCTURE FOR SATURN TANK WALL APPLICATION

    HUFFMAN, J. / LA IACONA, F. | AIAA | 1967
    Publisher: The American Institute of Aeronautics and Astronautics

    EVALUATION OF UNSTEADY AERODYNAMIC FORCES AND DYNAMIC RESPONSE OF FLEXIBLE AIRCRAFT STRUCTURE TO CONTINOUS TURBULANCE IN SUPERSONIC FLIGHT

    MORITO, JACK / SIDWELL, KENNETH | AIAA | 1967
    Publisher: The American Institute of Aeronautics and Astronautics

    A Working Conference: Fundamental Problems of Future Aerospace Structures

    M. B. Zisfein | NTIS | 1967
    Aerospace company representatives skilled in structure design, materials, and structural dynamics met in a working conference and set forth ...
    Keywords: Structural members , Composite materials

    Synthesis of structural damping.

    Bieber, R. E. / Chang, C. S. | NTRS | 1968
    Force deflection relationship under arbitrary loading for structure exhibiting hysteresis behavior ...
    Keywords: Structural Mechanics

    Fatigue loadings on commercial transport airplanes

    Coleman, T. L. / Hunter, P. A. | NTRS | 1969
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Structural Mechanics

    Coupling between structure and liquid propellants in a parallel-stage space shuttle design

    KANA, D. / KO, W. / FRANCIS, P. et al. | AIAA | 1972
    Publisher: The American Institute of Aeronautics and Astronautics

    Evaluation of a boron/epoxy reinforced titanium tubular truss for application to a space shuttle booster thrust structure

    CORVELLI, N. / CARRI, R. | AIAA | 1972
    Publisher: The American Institute of Aeronautics and Astronautics

    The spatial correlation method and a time-varying flexible structure

    WAN, F. / LAKSHMIKANTHAM, C. | AIAA | 1973
    Publisher: The American Institute of Aeronautics and Astronautics

    Computerized design of an outer planets spacecraft structure to survive the meteoroid environment

    KASE, P. | AIAA | 1973
    Publisher: The American Institute of Aeronautics and Astronautics

    Parametric studies of the wing flutter behavior of a STOL transport.

    Kyser, A. C. / Willis, C. M. | NTRS | 1973
    a four-engine STOL transport configuration having relatively low inplane wing stiffness and heavy engines. The wing structure was ...
    Publisher: NASA National Aeronautics and Space Administration

    Advanced composite lattice structure for improved structural integrity

    DOBYNS, A. / AVERY, J. / BLAISDELL, R. et al. | AIAA | 1974
    Publisher: The American Institute of Aeronautics and Astronautics

    Advanced Metallic Air Vehicle Structure Program

    BOENSCH, F. / HART, C. | AIAA | 1974
    Publisher: The American Institute of Aeronautics and Astronautics

    Air Superiority Fighter wing structure design for improved cost, weight and integrity

    FIGGE, F. / BERNHARDT, L. | AIAA | 1974
    Publisher: The American Institute of Aeronautics and Astronautics

    Optimal aeroelastic design of an oblique wing structure

    GWIN, L. | AIAA | 1974
    Publisher: The American Institute of Aeronautics and Astronautics

    Fatigue crack growth in diffusion bonded stiffened skin structure

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

    System identification of a complex structure

    BERMAN, A. | AIAA | 1975
    Publisher: The American Institute of Aeronautics and Astronautics

    Hypersonic wing test structure design, analysis, and fabrication

    PLANK, P. | AIAA | 1975
    Publisher: The American Institute of Aeronautics and Astronautics

      Hypersonic wing test structure design, analysis, and fabrication

      Plank, P. P. | NTRS | 1975
      , part of the wing (85 sq ft) was designed, fabricated, and assembled into a test structure to experimentally verify the structural adequacy of ...
      Publisher: NASA National Aeronautics and Space Administration
      Keywords: Aircraft Design, Testing And Performance

    Ion vapor deposited aluminum improves structure durability

    FANNIN, E. / STEUBE, K. | AIAA | 1975
    Publisher: The American Institute of Aeronautics and Astronautics

    A coupled fluid-structure dynamic analysis for water impact loads

    HERTING, D. | AIAA | 1975
    Publisher: The American Institute of Aeronautics and Astronautics

    Development of a mass optimized European communications satellite structure

    SCHNEITER, H. / SCHIBLI, U. / WIJKER, J. et al. | AIAA | 1975
    Publisher: The American Institute of Aeronautics and Astronautics