Dynamic Strain Sensors and Accelerometers for Structural Testing: Cases of Measurements on a Civil Structure and on the GVT of an F-16 Aircraft

Author:

Salzano C.

Publisher

Springer Nature Switzerland

Reference22 articles.

1. dos Santos, F.L., Peeters, B., Debille, J., Salzano, C., Desmet, W.: The use of dynamic strain sensors and measurements on the ground vibration testing of an F-16 Aircraft. In: Proceedings of IFASD 2015 International Forum on Aeroelasticity and Structural Dynamics (2015)

2. Dieckelman, R.J., Hauenstein, A.J., Ritzel, R.P.: The ground vibration test - a boeing ids perspective. In: Proceedings of IMAC-XXIII International Modal Analysis Conference (2005)

3. Göge, D., Böswald, M., Füllekrug, U., Lubrina, P.: Ground vibration testing of large aircraft state-of-the-art and future perspectives (2007)

4. Pickrel, C.R., Foss, G.C., Phillips, A.W., Allemang, R.J., Brown, D.L.: New concepts gvt. In: IMAC XXIV International Modal Analysis Conference (2006)

5. Bernasconi, O., Ewins, D.J.: Application of strain modal testing to real structures. In: Proceedings of the 7th International Modal Analysis Conference, vol. 2, pp. 1453–1464 (1989)

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