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Design and simulation of quadcopter mode system on hybrid UAV quadplane configuration
by
Marta, Aryandi
,
Muis, Abdul
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Conference Proceeding
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Data acquisition system in LSU-02 NG LD wing static test based on whiffletree
by
Marta, Aryandi
,
Wirawan, Nanda
,
Ardiansyah, Riki
,
Nugroho, Yudha Agung
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Wing static test of LSU-02 NGLD aircraft using Whiffletree method
by
Ula, Nur Mufidatul
,
Marta, Aryandi
,
Wijaya, Yusuf Giri
,
Muksin
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Conference Proceeding
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Flexural test characteristic of unidirectional carbon fiber-epoxy resin with 0o and 90o fiber alignment variation
by
Marta, Aryandi
,
Pratama, Mikhael Gilang Pribadi Putra
,
Vicarneltor, David Natanael
,
Rizkyta, Ara Gradiniar
,
Muzayadah, Nurul Lailatul
,
Ula, Nur Mufidatul
,
Nurtiasto, Taufiq Satrio
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Analysis of composite fuselage structure under axial impact loading
by
Wiranto, Ilham Bagus
,
Saraswati, Sherly Octavia
,
Prabowo, Aditya Rio
,
Al Fikri, Iqbal Reza
,
Chairunnisa
,
Muttaqie, Teguh
,
Adhynugraha, Muhammad Ilham
,
Megawanto, Fadli Cahya
,
Hidayat, Arif
,
Fuadi, Abid Paripurna
,
Marta, Aryandi
,
Wandono, Fajar Ari
,
Nurrohmad, Abian
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Procedia Structural Integrity
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Experimental studies on crashworthiness analysis of a sandwich composite panel under axial impact: A comprehensive review
by
Wiranto, Ilham Bagus
,
Saraswati, Sherly Octavia
,
Prabowo, Aditya Rio
,
Fikri, Iqbal Reza Al
,
Chairunnisa
,
Muttaqie, Teguh
,
Adhynugraha, Muhammad Ilham
,
Megawanto, Fadli Cahya
,
Hidayat, Arif
,
Paripurna, Abid
,
Marta, Aryandi
,
Wandono, Fajar Ari
,
Nurrohmad, Abian
Published in
Procedia Structural Integrity
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Procedia Structural Integrity
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Aluminum
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Finite Element Method
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Load Cells
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Physical Sciences
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