The Shock and Vibration Bulletin. Part 4. Dynamic Properties of Materials, Applications of Materials, Shock and Blast, Fragments
Abstract
Contents: Material Damping as a Means of Quantifying Fatigue Damage in Composites; Sonic Fatigue Testing of The NASA L-1011 Composite Aileron; Modeling a Temperature Sensitive Confined Cushioning System; Preliminary Hardness Evaluation Procedure For Identifying Shock Isolation Requirements; An Application of Tuned Mass Dampers to The Suppression of Severe Vibration in The Roof of an Aircraft Engine Test Cell; Comparison of Analytical and Experimental Results For a Semi-Active Vibration Isolator; An Experimental Investigation of Noise Attenuating Techniques For Space Shuttle Canisters; Dynamic Integrity Methods Including Damping For Electronic Packages in Random Vibration; Overview of Shock Analysis And Testing in The Federal Republic of Germany; Conservatism in Shock Analysis And Testing; Measurement of Dynamic Structural Characteristics of Massive Buildings by High-Level Multipulse Techniques; Consideration of an Optimal Procedure For Testing The Operability of Equipment Under Seismic Disturbances; Dynamic Loading of Metal Riveted Joints; Generalized Graphical Solution For Estimating Recoilless Rifle Breech Blast Overpressures And Impulses; Predicting The Motion of Flyer Plates Driven by Light-Initiated Explosive For Impulse Loading Experiments; Scaling of Initiation of Explosives by Fragment Impact; Equations For Determining Fragment Penetration And Perforation Against Metals; Breaching of Structural Steel Plates Using Explosive Disks.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1980
- Accession Number
- ADA186635
Entities
Organizations
- United States Naval Research Laboratory