This paper first summarises analytical equations which govern the dynamic behaviour of elastomechanical structures under base excitation. Special attention is focused on the dynamics at the interface between the vibration table and test structure. The dynamic relations at the interface are explained with particular consideration to the interface forces. An example of an interface forcing function is shown and discussed. A suitable device for force measurements (FMD) is described. It was specifically designed for themeasurement of the six dynamic interface forces and moments between a shaker table and a tested structure. The FMD was recently utilised for base-driven tests on a liquid propellant tank and support structure. The test set...
The dynamic qualification of space structures today is performed by means of driven base tests in or...
Increase of size and recent advances in lightweight design of space systems have led to the requirem...
The increase of dimensions and recent advances in the lightweight design of space systems have led t...
This paper concentrates on the fundamentals of the structural vibration behaviour of a structure und...
Most of the commonly used modal testing methods are based on multiple point excitation. An alternat...
Most of the commonly used modal testing methods are based on multiple point excitation. The interfa...
The force-limited vibration test approaches discussed in NASA-7004C were developed to reduce overtes...
Vibration testing, techniques have been developed and employed that reduce the overtesting caused by...
This paper deals with the identification of effective masses and modal masses from base-driven tests...
The Force Measurement Device (FMD) is used for the measurement of interface forces between an electr...
In vibration tests, the behavior of the structure depends on its mechanical boundary conditions, whi...
Modern machines are often composed of components that are designed and manufactured by a number of s...
The conventional dynamic qualification of space structures requires the availability of base-driven ...
The dynamic response of coupled structures is influenced by the mechanical joints connecting the ind...
The increase of dimensions and recent advances in lightweight design of space systems have led to th...
The dynamic qualification of space structures today is performed by means of driven base tests in or...
Increase of size and recent advances in lightweight design of space systems have led to the requirem...
The increase of dimensions and recent advances in the lightweight design of space systems have led t...
This paper concentrates on the fundamentals of the structural vibration behaviour of a structure und...
Most of the commonly used modal testing methods are based on multiple point excitation. An alternat...
Most of the commonly used modal testing methods are based on multiple point excitation. The interfa...
The force-limited vibration test approaches discussed in NASA-7004C were developed to reduce overtes...
Vibration testing, techniques have been developed and employed that reduce the overtesting caused by...
This paper deals with the identification of effective masses and modal masses from base-driven tests...
The Force Measurement Device (FMD) is used for the measurement of interface forces between an electr...
In vibration tests, the behavior of the structure depends on its mechanical boundary conditions, whi...
Modern machines are often composed of components that are designed and manufactured by a number of s...
The conventional dynamic qualification of space structures requires the availability of base-driven ...
The dynamic response of coupled structures is influenced by the mechanical joints connecting the ind...
The increase of dimensions and recent advances in lightweight design of space systems have led to th...
The dynamic qualification of space structures today is performed by means of driven base tests in or...
Increase of size and recent advances in lightweight design of space systems have led to the requirem...
The increase of dimensions and recent advances in the lightweight design of space systems have led t...