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<title><![CDATA[PENGUJIAN CRASHWORTHINESS HONEYCOMB SANDWICH DENGAN VARIASI JUMLAH LAPISAN INTI MENGGUNAKAN SOFTWARE ANSYS]]></title>
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<note>Crashworthiness juga dapat dipahami sebagai ketahanan kehanhancuran material yang berkelanjutan serta mempertahankan beberapa bagian material pasca penghancuran. Material yang baik digunakan untuk crashworthiness adalah material yang memiliki sifat ulet salah satunya yaitu polimer. Polimer dapat meningkat kekuatannya jika dikombinasikan dengan material lain menjadi komposit. Struktur honeycomb sandwich (sarang lebah) merupakan salah satu jenis komposit. Tujuan dari penelitian ini yaitu modeling struktur panel honeycomb sandwich two directional trapezoidal wave core dengan bahan dasar epoxy resin glass fiber woven rope. Pengujian ini dilakukan untuk mengetahui maksimum defleksi yang terjadi dan energi maksimum yang dapat diserap oleh honeycomb sandwich dengan bantuan software ansys. honeycomb sandwich 1 lapis inti, maksimum defleksi yang terjadi sebesar 11,15 mm dengan waktu yang dibutuhkan sebesar 0,0030 s dan pada pengujian honeycomb sandwichi 1 lapis inti maksimum energi yang dapat diserap sebesar 106,85 J pada waktu 0,0030 s.</note>
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