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    STRUCTURAL DYNAMICS ASPECTS OF THE GEMINI PRCGRAM

    CALLAHAN, J. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Advanced composite material application to aircraft structures

    ROGERS, CHARLES | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    SYSTEMS EVALUATION GF ADVANCED STRUCTURES AND MATERIALS IN FUTURE LAUNCH VEHICLES

    BODDY, JOHN / MITCHELL, JAMES / HARRIS, LEONARD | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    STEADY STATE DYNAMICS OF LARGE SPINNING NET CONFIGURATION STRUCTURES

    YU, SHAN / TABER, JOHN | AIAA | 1967
    Verlag: 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 ...
    Schlagwörter: Structural members , Composite materials

    PRESSURE SHZLL STRUCTURES FOR SPACE

    MARVIN, R. / HAMMER, E. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    PRINCIPLE OF MAXIMUM ENTROPY AND ITS APPLICATION IN RELIABILITY ESTIMATION OF AIRCRAFT STRUCTURES

    SHAH, HARESH | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    A FINITE ELEMENT APPROACH FOR THE ANALYSIS OF RANDOMLY EXCITED COMPLEX ELASTIC STRUCTURES

    NEWSOM, C. / FULLER, J. / SHERRER, R. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    DISCRETE ELEMENT METHODS FOR THE PLASTIC ANALYSIS OF STRUCTURES SUBJECTED TO CYCLIC LOADING

    ARMEN, JR., H. / ISAKSON, G. / PIFKO, A. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    THE EFFECT OF FIBER SPACING IN COMPOSITES ON MODULUS OF LAMINATE CONFIGURATIONS USED IN AEROSPACE STRUCTURES

    BERG, K. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Comparison of integrally formed compression panel efficiencies with other aerospace panel concepts

    McClaren, S.W. / McQueen, J.C. / Martin, A.P. | Engineering Index Backfile | 1967
    Examples of structures include conventional sheet-stringer panels, honeycomb panels, integrally machined and stiffened panels, trusscore ...
    Schlagwörter: Rockets and missiles

    Status of reentry vehicle heatshields

    Channon, S.L. / Barry, W.T. | Engineering Index Backfile | 1967
    influence selection of materials for heat shield application are vehicle configuration, ballistic coefficient, re-entry velocity and flight ...

    Space evacuation of NRC-2 insulation for liquid hydrogen tankage.

    Crawford, R. F. / Hannah, R. G. / Nevins, C. D. | NTRS | 1967
    Space evacuation of NRC-2 insulation for liquid hydrogen tankage, noting vacuum test apparatus and cold plate test ...
    Verlag: JOURNAL OF SPACECRAFT AND ROCKETS, VOL. 4, P. 1598-1602.
    Schlagwörter: Thermodynamics And Combustion

    Optimal control of maneuver-induced vibration in flexible aerospace vehicles

    Karnopp, D. | Engineering Index Backfile | 1967
    ; some typical thrust patterns are examined which accomplish desired maneuver and also are constrained to leave some vibratory modes unexcited at ...

    AIAA/ASME 9th structures, structural dynamics and materials conference

    Engineering Index Backfile | 1968
    Twenty-four papers deal with applications in fields of aerospace vehicle design and shell structures; individual papers are abstracted ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA)
    Schlagwörter: Structural design

    The effects of hypervelocity impact on honeycomb structures

    LATHROP, B. / SENNETT, R. | AIAA | 1968
    Verlag: The American Institute of Aeronautics and Astronautics

    Finite element analysis of inelastic structures

    BLACKLOCK, J. / RICHARD, R. | AIAA | 1968
    Verlag: The American Institute of Aeronautics and Astronautics

    The tensile strength of glass-reinforced composite structures

    BLAKE, R. | AIAA | 1968
    Verlag: The American Institute of Aeronautics and Astronautics

    Material design concepts for urban transport aircraft

    MacNeill, C.E. | Engineering Index Backfile | 1968
    fracture toughness, creep, and fatigue properties; composite materials offer improved service use by providing freedom from deterioration and ease ...
    Schlagwörter: Aircraft materials

    Synthesis of structural damping.

    Bieber, R. E. / Chang, C. S. | NTRS | 1968
    Schlagwörter: Structural Mechanics