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
194 pages
Report
No indication
English
Structural Mechanics , Manned Spacecraft , Aircraft , Shock(Mechanics) , Vibration , Symposia , Aerospace craft , Test methods , Experimental data , Strain(Mechanics) , Instrumentation , Measurement , Dynamic tests , Remotely piloted vehicles , Acoustics , Aerodynamics , Mass , Transport aircraft , Sonic fatigue , Ground support equipment , Vibroacoustics , Aeroacoustics
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