In this paper, the use of advanced, flexible shaker excitation signals will be investigated with the aim (1) to obtain improved Frequency Response Function (FRF) estimations and (2) to assess the non-linearities of the excited system / structure. Pseudo-random and more general multisine signals rather than the more traditional pure or burst random signals will be used to increase the accuracy of the FRF estimate. Moreover, special multisine data acquisition and processing methods to identify the level of non-linearity will be illustrated by means of numerical simulation and real ground vibration testing on an aircraft scale model. The presented methods allow assessing the non-linearities at a single excitation level, which is in contrast to...
In modal testing, the force transducer and accelerometer mounted on the test structure will introduc...
Electronic equipments in flexible slender aerospace structures are subjected to severe vibration env...
The vibration characteristics of aerospace structures are investigated in so-called ground vibration...
The need to reduce testing time without diminishing the quality of the data is an important driver f...
Although they are generally modelled as linear systems, aircraft structures are known to be prone to...
In this paper, we discuss optimized strategies to measure the frequency response function in the pre...
An experiment is designed to identify input-output relations of a mechanical positioning system with...
The modal identification of large and dynamically complex structures often requires a multi-point ex...
The European aircraft industry is constantly calling for a reduction in the testing time of new airc...
Ground vibration tests (GVTs) in Europe nowadays combine the benefits of the very reliable but time ...
Higher-order frequency response functions (FRFs) are important to the analysis and identification of...
Experimental simulations of random excitations are nowadays performed digitally by applying the Inve...
Ground vibration tests (GVTs) on aircraft prototypes are mainly performed to identify experimentally...
Ground vibration tests (GVTs) on aircraft prototypes are mainly performed to experimentally identify...
Shock and vibration testing of railway applications is regulated by the European Norm EN 61373. With...
In modal testing, the force transducer and accelerometer mounted on the test structure will introduc...
Electronic equipments in flexible slender aerospace structures are subjected to severe vibration env...
The vibration characteristics of aerospace structures are investigated in so-called ground vibration...
The need to reduce testing time without diminishing the quality of the data is an important driver f...
Although they are generally modelled as linear systems, aircraft structures are known to be prone to...
In this paper, we discuss optimized strategies to measure the frequency response function in the pre...
An experiment is designed to identify input-output relations of a mechanical positioning system with...
The modal identification of large and dynamically complex structures often requires a multi-point ex...
The European aircraft industry is constantly calling for a reduction in the testing time of new airc...
Ground vibration tests (GVTs) in Europe nowadays combine the benefits of the very reliable but time ...
Higher-order frequency response functions (FRFs) are important to the analysis and identification of...
Experimental simulations of random excitations are nowadays performed digitally by applying the Inve...
Ground vibration tests (GVTs) on aircraft prototypes are mainly performed to identify experimentally...
Ground vibration tests (GVTs) on aircraft prototypes are mainly performed to experimentally identify...
Shock and vibration testing of railway applications is regulated by the European Norm EN 61373. With...
In modal testing, the force transducer and accelerometer mounted on the test structure will introduc...
Electronic equipments in flexible slender aerospace structures are subjected to severe vibration env...
The vibration characteristics of aerospace structures are investigated in so-called ground vibration...