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Abstract— Smoothed Particle Hydrody

Abstract— Smoothed Particle Hydrodynamics (SPH) is used to
model the ditching of a helicopter. Helicopters have a high
centre of gravity, are not integrally watertight so tend to roll over
and sink within seconds of landing on the water surface. Modern
helicopters employ Emergency Flotation Systems (EFS) that are
essentially large air-bags to provide increased buoyancy and
stability to the helicopter, thereby enhancing occupant survival
rates. A hybridised finite element code that includes SPH
elements, rigid finite elements, flexible finite elements, sliding
contact interface algorithms and air-bag simulation tools from
the automotive industry is used to demonstrate the behaviour of
the complex fluid-structure interaction scenario of a helicopter
landing on water with and without inflating air-bags.
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Hasil (Bahasa Indonesia) 1: [Salinan]
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Abstract— Smoothed Particle Hydrodynamics (SPH) is used tomodel the ditching of a helicopter. Helicopters have a highcentre of gravity, are not integrally watertight so tend to roll overand sink within seconds of landing on the water surface. Modernhelicopters employ Emergency Flotation Systems (EFS) that areessentially large air-bags to provide increased buoyancy andstability to the helicopter, thereby enhancing occupant survivalrates. A hybridised finite element code that includes SPHelements, rigid finite elements, flexible finite elements, slidingcontact interface algorithms and air-bag simulation tools fromthe automotive industry is used to demonstrate the behaviour ofthe complex fluid-structure interaction scenario of a helicopterlanding on water with and without inflating air-bags.
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Hasil (Bahasa Indonesia) 2:[Salinan]
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Abstrak merapikan Partikel Hidrodinamika (SPH) digunakan untuk
memodelkan membolos dari helikopter. Helikopter memiliki tinggi
pusat gravitasi, tidak integral kedap sehingga cenderung berguling
dan tenggelam dalam hitungan detik dari mendarat di permukaan air. Modern
helikopter mempekerjakan Sistem Flotation Darurat (EFS) yang
pada dasarnya udara-tas besar untuk memberikan peningkatan daya apung dan
stabilitas helikopter, sehingga meningkatkan kelangsungan hidup penghuni
tarif. Kode elemen hingga hibrid yang mencakup SPH
elemen, elemen hingga kaku, elemen hingga fleksibel, geser
algoritma antarmuka kontak dan alat-alat udara-tas simulasi dari
industri otomotif digunakan untuk menunjukkan perilaku
kompleks cairan-struktur skenario interaksi helikopter
mendarat di atas air dengan dan tanpa menggembungkan udara-tas.
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