Contents: An experimental/analytical determination of transporter loads on the Viking Spacecraft; Determination of propellant effective mass properties using modal test data; Unique flight instrumentation/data reduction techniques employed on the Viking dynamic simulator; Analytical prediction and correlation for the orbiter during the Viking Spacecraft sinusoidal vibration test; Fail safe forced vibration testing of the Viking 1975 developmental spacecraft; A method for determining tactical missile joint compliances from dynamic test data; Dynamic strain measurement techniques at elevated temperatures; An active linear bridge for strain measurement; Viking dynamic simulator vibration testing and analysis method; Analysis and flight test correlation of vibroacoustic environments on a remotely piloted vehicle; Aero-acoustic environment of rectangular cavities with length to depth ratios in the range of four to seven; Prediction of acoustically induced vibration in transport aircraft; Simplified techniques for predicting vibro-acoustic environments; and Use of a semi-periodic structural configuration for improving the sonic fatigue life of stiffened structures.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    The Shock and Vibration Bulletin. Part 3. Aerospace Vehicles, Vibro-Acoustics


    Erscheinungsdatum :

    1975


    Format / Umfang :

    195 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch