The behaviour of an airframe with f

The behaviour of an airframe with flexible pontoons in
impacting and floating on water is a complex phenomenon.
The explicit finite element code PAM-CRASH with its SPH
solver has already been shown [1,2] to successfully simulate
various scenarios involving fluid-structure interaction (FSI).
The dynamics of a helicopter ditching with a rigid EFS has
previously been demonstrated [3]. The development in this
paper exploits the (automotive) occupant safety airbag model
within the aforementioned code to approximate the inflation of
large flexible pontoons, facilitating the simulation of ditching
of helicopters fitted with an EFS.

Hasil (Bahasa Indonesia) 1:

Perilaku airframe dengan fleksibel ponton diberdampak dan mengambang di air adalah fenomena yang kompleks.Kode eksplisit metoda unsur PAM-CRASH dengan SPH nyaSolver telah sudah terbukti [1,2] berhasil mensimulasikanberbagai skenario yang melibatkan cairan-struktur interaksi (FSI).Dinamika helikopter membolos dengan EFS kaku telahsebelumnya telah menunjukkan [3]. Perkembangan inikertas eksploitasi (otomotif) penghuni keselamatan airbag modeldalam kode tersebut untuk perkiraan inflasibesar ponton fleksibel, memfasilitasi simulasi memboloshelikopter dilengkapi dengan EFS.