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.
The Shock and Vibration Bulletin. Part 3. Aerospace Vehicles, Vibro-Acoustics
1975
195 pages
Report
No indication
English
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