Thesis on the reduction of vibrations at the launcher / payload interface in cooperation with EADS-ST. DPAC / SPAé contract : reduction of internal noise in helicopters...
Internal Noise Prediction in Fixed-Wing Aircraft Fuselages - ONERA / DADS-ENWho are we ?Internal Vibroacoustics in the LF, MF and HF Range... Internal Noise Prediction of Internal Noise in Fixed-Wing Aircraft Fuselages. The DADS department at ONERA is involved in the development of numerical tools for the prediction of internal noise in aerospace structures..
