Vibration environment estimation and prediction is required for the aerospace vehicle during the initial phase of an aerospace equipment program in order to support design and procurement specifications. For many aerospace systems, acoustically driven random vibration represents the most significant vibration environment. Numerous procedures have been developed by individuals in the vibration field. A brief review of the estimation and prediction techniques developed in the past few decades for random vibration levels have been presented in this report focusing attention on aerospace vehicles and in particular on missile structures. (Author
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
Determination of the stresses and displacements which occur in response to random excitations cannot...
This paper presents a deterministic theory for the random vibration problem for predicting the respo...
The design of launch pad structures, particularly those having a large area-to-mass ratio, is govern...
Random vibration is the phenomenon wherein random excitation applied to a mechanical system induces ...
A method of predicting broadband random vibration criteria for components on space vehicles is prese...
This paper examines the prediction of National Space Transportation System (NSTS) payload random vib...
Flight equipment is exposed to random vibration excitations during launch and is functionally design...
AbstractAircraft vibration response environment prediction, which is adopted in aircraft initial veh...
The use of random signal analysis in vibration and structural analysis is discussed and documented. ...
Random Vibrations: Theory and Practice covers the theory and analysis of mechanical and structural s...
This paper deals with three procedures that are used to13; predict the response characterstics of Ae...
The random vibration analysis of aircraft structural components is often performed with simplified t...
To prevent over-testing of the load during the random vibration test an adaptation of the random bas...
The purpose of this thesis is to study the failure prediction of structures subjected to random vibr...
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
Determination of the stresses and displacements which occur in response to random excitations cannot...
This paper presents a deterministic theory for the random vibration problem for predicting the respo...
The design of launch pad structures, particularly those having a large area-to-mass ratio, is govern...
Random vibration is the phenomenon wherein random excitation applied to a mechanical system induces ...
A method of predicting broadband random vibration criteria for components on space vehicles is prese...
This paper examines the prediction of National Space Transportation System (NSTS) payload random vib...
Flight equipment is exposed to random vibration excitations during launch and is functionally design...
AbstractAircraft vibration response environment prediction, which is adopted in aircraft initial veh...
The use of random signal analysis in vibration and structural analysis is discussed and documented. ...
Random Vibrations: Theory and Practice covers the theory and analysis of mechanical and structural s...
This paper deals with three procedures that are used to13; predict the response characterstics of Ae...
The random vibration analysis of aircraft structural components is often performed with simplified t...
To prevent over-testing of the load during the random vibration test an adaptation of the random bas...
The purpose of this thesis is to study the failure prediction of structures subjected to random vibr...
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
Determination of the stresses and displacements which occur in response to random excitations cannot...
This paper presents a deterministic theory for the random vibration problem for predicting the respo...