The Shock and Vibration Bulletin. Part 3. Aerospace Vehicles, Vibro-acoustics
Abstract
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1975
- Accession Number
- ADA112619
Entities
People
- A. F. Leondis
- F. D. Day
- George Kachadourian
- Gerald R. Brownlee
- James W. Fortenberry
- Jay C. Chen
- John G. Maloney
- Paul T. Jaquay
- R. C. Taylor
Organizations
- United States Naval Research Laboratory