The Shock and Vibration Bulletin. Part 3. Structural Analysis, Fatigue.
Abstract
Partial contents: Structural Analysis -- A source of large errors in calculating system frequencies; Research method of the eigenmodes and generalized elements of a linear mechanical structure, Calculation of natural frequencies and mode shapes of mass loaded aircraft structures, Rocket motor response to transverse blast loading, Experimental and theoretical dynamic analysis of carbon-graphite composite shells, Use of shock spectra to evaluate jitter of a flexible maneuvering spacecraft, Buckling of Euler's rod in the presence of ergodic random damping, Wave propagation in a cylindrical shell with joint discontinuity, Response to moving loads over a crystalline half-space, Adjustment of a conservative non gyroscopic mathematical model from a measurement, and First-passage failure probability in random vibration of structures with random properties; Fatigue -- Fracture mechanics applied to step-stress fatigue under sine/random vibration, and Random fatigue damage approach to machinery maintenance.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1978
- Accession Number
- ADA148084
Entities
Organizations
- United States Naval Research Laboratory