Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Nur Mufidatul Ula"'
Autor:
Muksin Muksin, Mikhael Gilang Pribadi P. Pratama, Yudha Agung Nugroho, Yusuf Giri Wijaya, Nur Mufidatul Ula, Adi Wirawan
Publikováno v:
Jurnal Ilmu Dasar, Vol 23, Iss 1, Pp 75-80 (2022)
Vibration testing on telemetry system payload is needed to determine its resistance to vibration during operation. Vibration testing of telemetry system payloads requires a test fixture. Test fixture is used to transmit vibration from shaker to telem
Externí odkaz:
https://doaj.org/article/957e752ad0f14589bf3c33a3d10eacde
Publikováno v:
Computational and Experimental Research in Materials and Renewable Energy, Vol 4, Iss 1, Pp 21-29 (2021)
LSU-05 NG is one of the unmanned air vehicles (UAV) developed by the aviation technology center LAPAN. The LAPAN aviation technology center designed the LSU-05 NG to be able to carry a larger payload and broader range than other types of LSUs. Theref
Externí odkaz:
https://doaj.org/article/140f5f397afb4c05b04548199680b31b
Autor:
Nur Mufidatul Ula, Yusuf Giri Wijaya, Muksin, P.P.P. Mikhael Gilang, Nurul Lailatul Muzayadah, Redha Akbar Ramadhan
Publikováno v:
Measurement: Sensors, Vol 18, Iss , Pp 100230- (2021)
Vibration testing has carried out on the sandwich material composite specimen. This study aimed to determine the vibration characteristics of carbon-based sandwich composites. Sandwich composites were made by using the Vacuum assisted resin infusion
Externí odkaz:
https://doaj.org/article/445097b2bb154501b83af547b5796ff0
Publikováno v:
Technologic. 12
Fixture uji vibrasi harus dapat memegang device under test (DUT) selama proses pengujian dan sesuai dengan kondisi aslinya. Umumnya fixture uji vibrasi yang dibuat harus sesuai dengan geometri DUT. Oleh karena fixture uji vibrasi dibuat secara khusus
Autor:
Nur Mufidatul Ula, Yusuf Giri Wijaya, Mikhael Gilang Pribadi Putra Pratama, Nurul Lailatul Muzayadah
Publikováno v:
Technologic. 12
Material Komposit Sandwich adalah jenis komposit yang terdiri dari susunan komposit laminate dengan core didalamnya. Pemanfaatan komposit sandwich saat ini sangat luas termasuk salah satunya sebagai struktur sekunder dalam pesawat mengingat masa komp
Autor:
Yusuf Giri Wijaya, Agus Harno Nurdin Syah, Nur Mufidatul Ula, Mikhael Gilang Pribadi Putra Pratama, Muksin Muksin
Publikováno v:
Angkasa: Jurnal Ilmiah Bidang Teknologi. 12
Vibration testing of the head expander has been carried out. This test aims to determine the dynamic characteristics of the head expander that used in the Laboratory of Temperature and Vibration Testing, The Aeronautics Technology-LAPAN. The Head exp
Autor:
Nurul Lailatul Muzayadah, Redha Akbar Ramadhan, Muksin, Yusuf Giri Wijaya, P.P.P. Mikhael Gilang, Nur Mufidatul Ula
Publikováno v:
Measurement: Sensors, Vol 18, Iss, Pp 100230-(2021)
Vibration testing has carried out on the sandwich material composite specimen. This study aimed to determine the vibration characteristics of carbon-based sandwich composites. Sandwich composites were made by using the Vacuum assisted resin infusion
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811509490
The use of composite materials in UAV development has increased significantly. The chosen of composite material for the UAV structure is due to the advantage of composite both from the strength and the light side of material that good for improving s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6a30ec8881f5188441f70139814ff90d
https://doi.org/10.1007/978-981-15-0950-6_57
https://doi.org/10.1007/978-981-15-0950-6_57
Publikováno v:
AIP Conference Proceedings.
Wings of LSU-02 NGLD has been tested using the Whiffletree method. The LSU-02 NGLD wing consists of spars made of aluminum, ribs made of balsa wood and skin made of composite material consisting of Balsa, Epoxy and E glass wood. This study aims to de
Autor:
Angga Septiyana, Ardian Rizaldi, Eries Bagita Jayanti, Kurnia Hidayat, Novita Atmasari, Prasetyo Ardi Probo Suseno, Redha Ramadhan Akbar, Nur Mufidatul Ula, Mohamad Luthfi Ramadiansyah
Publikováno v:
Jurnal Teknologi Dirgantara. 17:109
Penelitian ini berfokus pada analisa penentuan power loading pada awal desain pesawat LSU-05 NG. Dengan menentukan power loading maka kebutuhan daya engine untuk pesawat LSU-05 NG dapat diestimasi. Artinya pemilihan engine dapat dilakukan sehingga me