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Synonyms were used for: Conference • Dynamics • Materials • Structural Dynamics
Search without synonyms: title: 31st Structures, Structural Dynamics and Materials Conference

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    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 ...
    Publisher: JOURNAL OF SPACECRAFT AND ROCKETS, VOL. 4, P. 1598-1602.
    Keywords: Thermodynamics And Combustion

    Synthesis of structural damping.

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

    Structural synthesis of integrally stiffened cylinders.

    Kicher, T. P. | NTRS | 1968
    Structural design of stiffened cylindrical shells, discussing minimum weight, prevention of buckling modes, etc ...
    Publisher: JOURNAL OF SPACECRAFT AND ROCKETS, VOL. 5, P. 62-67.
    Keywords: Structural Mechanics

    Analyses of the Longitudinal Dynamics of Launch Vehicles with Application to a 1/10- Scale Saturn V Model

    Leonard, H. W. / Pinson, L. D. / Raney, J. P. | NTRS | 1968
    Publisher: JOURNAL OF SPACECRAFT AND ROCKETS, VOL. 5, P. 303-308.

    Analysis of curved thin-walled shells of revolution.

    Kalnins, A. | NTRS | 1968
    Keywords: Structural Mechanics

    Stress corrosion cracking of titanium alloys.

    Beck, T. R. / Blackburn, M. J. | NTRS | 1968
    Stress corrosion cracking of titanium alloys noting tensile test data, crack propagation in salt solution and in pure solvents and ...
    Keywords: Materials, Metallic

    Concepts for more efficient bulkhead designs for launch and space vehicles.

    Bernstein, A. I. / Blumrich, J. F. | NTRS | 1968
    Low profile bulkheads for launch vehicles and spacecraft compartments to obtain structural weight reduction ...
    Publisher: NASA National Aeronautics and Space Administration

    A mathematical model for flexible response of uprated Saturn I to inflight winds.

    Mitchell, H. P. / Wells, C. R. | NTRS | 1968
    Publisher: JOURNAL OF SPACECRAFT AND ROCKETS, VOL. 5, P. 313-320.

    Evaluation of aerothermoelasticity problems for unmanned Mars-entry vehicles.

    Houbolt, J. C. / Menkes, E. G. | NTRS | 1969
    Aerothermoelasticity problems for Mars entry vehicles, discussing deceleration loads, separated hot gas flow, shield thermal gradients and ...
    Publisher: NASA National Aeronautics and Space Administration

    Monte Carlo dynamic analysis for lunar module landing loads

    Merchant, D. H. / Sawdy, D. T. | NTRS | 1971
    Apollo lunar module structural integrity for lunar landing verified by Monte Carlo dynamic analysis ...
    Publisher: NASA National Aeronautics and Space Administration

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