The demand on safety performance of launching structure and equipment system from impulsive excitations necessitates a study which predicts the maximum response of the system as well as the maximum stresses in the system. A method to extract higher modes and frequencies for a class of multiple degree-of-freedom (MDOF) Structure system is proposed. And, along with the shock spectra derived from a linear oscillator model, a procedure to obtain upper bound solutions for maximum displacement and maximum stresses in the MDOF system is presented
Dynamic responses of a series of typical three-degree of freedom structures to strong-motion earthqu...
Unlike an earlier shock spectra approach, generalization permits an accurate elastic interaction bet...
Component requirements govern design and production in the aerospace industry. One such potential re...
University of Minnesota Ph.D. dissertation. 2015. Major: Mechanical Engineering. Advisor: Susan Mant...
A method to determine a bound of structural loads for a spacecraft mounted on a launch vehicle is de...
The results of a research task to investigate the capabilities of electrodynamic vibrators (shakers)...
The operation of dynamical systems in harsh environments requires continuous monitoring. Internal se...
As it is stated in the ISO 18431-4 Standard, a Shock Response Spectrum is defined as the response to...
The proceedings of the 58th Shock and Vibration Symposium, held in Huntsville, Alabama, October 13 ...
Study of the shock and vibration response of a multistage structure employed analytically, lumped-ma...
[[abstract]]Due to its simplicity, shock response spectrum has become widely used as a means of desc...
The initiating explosive shock environment of an aerospace mission has the characteristics of instan...
Because of its simplicity, the shock response spectrum has become widely used as a means of describi...
Spacecraft systems and sub/systems are subject to high mechanical energy at a high frequency during ...
It is common to establish shock and vibration design and/or test criteria for equipment mounted on a...
Dynamic responses of a series of typical three-degree of freedom structures to strong-motion earthqu...
Unlike an earlier shock spectra approach, generalization permits an accurate elastic interaction bet...
Component requirements govern design and production in the aerospace industry. One such potential re...
University of Minnesota Ph.D. dissertation. 2015. Major: Mechanical Engineering. Advisor: Susan Mant...
A method to determine a bound of structural loads for a spacecraft mounted on a launch vehicle is de...
The results of a research task to investigate the capabilities of electrodynamic vibrators (shakers)...
The operation of dynamical systems in harsh environments requires continuous monitoring. Internal se...
As it is stated in the ISO 18431-4 Standard, a Shock Response Spectrum is defined as the response to...
The proceedings of the 58th Shock and Vibration Symposium, held in Huntsville, Alabama, October 13 ...
Study of the shock and vibration response of a multistage structure employed analytically, lumped-ma...
[[abstract]]Due to its simplicity, shock response spectrum has become widely used as a means of desc...
The initiating explosive shock environment of an aerospace mission has the characteristics of instan...
Because of its simplicity, the shock response spectrum has become widely used as a means of describi...
Spacecraft systems and sub/systems are subject to high mechanical energy at a high frequency during ...
It is common to establish shock and vibration design and/or test criteria for equipment mounted on a...
Dynamic responses of a series of typical three-degree of freedom structures to strong-motion earthqu...
Unlike an earlier shock spectra approach, generalization permits an accurate elastic interaction bet...
Component requirements govern design and production in the aerospace industry. One such potential re...