1–50 of 1,434 hits
|

    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

    Isogrid structures

    Slysh, P. / Dyer, J. E. / Furman, J. H. et al. | NTRS | 1975
    Test results and related structural instability analyses are presented for a 10-foot-diameter, 37-inch-long cylinder, and a 10-foot ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Structural Mechanics

    Design of a graphite/epoxy metering truss for the Large Space Telescope

    Oken, S. / Skoumal, D. E. / Straayer, J. W. et al. | NTRS | 1975
    This paper presents the design development of a truss-type structure which utilizes graphite/epoxy as the primary material system. A review ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    DEVELOPMENT OF A GRAPHITE REINFORCED THERMOPLASTIC DESIGN CONCEPT FOR A TARGCT DRONE AIRCRAFT FUSELAGE STRUCTURE APPLICATION

    LAAKSO, J. / HOGGATT, J. | AIAA | 1976
    Publisher: The American Institute of Aeronautics and Astronautics

    A mixed method of analysis for vehicle structure

    NI, C.-M. / LIN, K.-H. | AIAA | 1977
    Publisher: The American Institute of Aeronautics and Astronautics

    Development of brazed Rene 41 honeycomb structure

    ARNQUIST, J. / HEPLER, A. | AIAA | 1978
    Publisher: The American Institute of Aeronautics and Astronautics

    NASA/FAA general aviation crash dynamics program - A status report

    Thomson, R. G. / Goetz, R. C. | NTRS | 1979
    The objective of the Langley Research Center general aviation crash dynamics program is to develop technology for improved crash safety and ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Aircraft Design, Testing And Performance

    Combined use of upper bound theorems and available lower bound information<149>for plastic structure deformation under impact loads

    NYSTROM, G. | AIAA | 1979
    Publisher: The American Institute of Aeronautics and Astronautics

    A method of order reduction for structural dynamics

    ANDERSON, L. / HALLAUER, JR., W. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Topics of major importance for the structural design/analysis/construction of the Mark II hydrofoil craft hull structure

    WHITMAN, JR., B. / PAYNE, K. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Integrated thermal-structural finite element analysis

    THORNTON, E. / DECAHAUMPHAI, P. / WIETING, A. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Cyclic plasticity and failure of structural components

    AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Structural sizing considerations for large space platforms

    HEARD, JR., W. / BUSH, H. / WALZ, J. et al. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Structural analysis and test Space Shuttle Orbiter window system

    DOTE, H. / THEODORE, K. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Turbine blade structural dynamic analysis

    DICKERSON, E. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Improved methods for large scale structural synthesis

    PAPPAS, M. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    An attractive method for displaying material damping data

    JONES, D. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Advanced composite structure repair guide

    BECK, C. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Composite materials in a simulated space environment

    TENNYSON, R. | AIAA | 1980
    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

    Recovered transient load analysis for payload structural systems

    CHEN, J. / GARBA, J. / ZAGZEBSKI, K. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Structural design loads for future airplanes

    MILNS, P. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Release-rate calorimetry of multilayered materials for aircraft seats

    FEWELL, L. / PARKER, J. / DUSKIN, F. 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

    Damage tolerant design and test considerations in the engine structural integrity program

    COWIE, W. / STEIN, T. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Elevated temperature structural testing of advanced missiles

    OTTO, O. / INUKAI, G. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    On the dynamics of an axially moving beam submerged in a fluid

    TALEB, I. / MISRA, A. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Recovered transient load analysis for payload structural systems

    Chen, J. C. / Zagzebski, K. P. / Garba, J. A. | NTRS | 1980
    the information on a new payload structure to be launched by an identical launch vehicle. The advantage of the proposed method is that the ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    Unsteady aerodynamics of conventional and supercritical airfoils

    DAVIS, S. / MALCOLM, G. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Large space structures - Fantasies and facts

    CARD, M. / BOYER, W. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics