Zobrazeno 1 - 10
of 23
pro vyhledávání: '"Sayuti Syamsuar"'
Autor:
Sayuti Syamsuar, Karyawan, Hendrato, Yudiawan Fajar Kusuma, Muhammad, Sulistiya, Annissa Roschyntawati, Daif Rahuna, Widyawasta, Baharuddin Ali, Sutiyo, Bagiyo Suwasono
Publikováno v:
Data in Brief, Vol 51, Iss , Pp 109805- (2023)
Most seaplanes used for aircraft operations in territorial waters are classified into three main types, namely floatplanes, flying boats, and amphibians. Among these, the floatplane stands out as it replaced its landing gear with two floating pontoon
Externí odkaz:
https://doaj.org/article/e45c7d7d6db24a0caaf93692f0b7b2e7
Autor:
Sayuti Syamsuar, null Erwandi, Bagiyo Suwasono, null Sutiyo, Nina Kartika, Adityo Suksmono, Annissa Roshyntawati, null Hendrato, Andi M. Kadir, Arief Setyawan, Ali Munazid
Publikováno v:
PROCEEDINGS OF THE SYMPOSIUM ON ADVANCE OF SUSTAINABLE ENGINEERING 2021 (SIMASE 2021): Post Covid-19 Pandemic: Challenges and Opportunities in Environment, Science, and Engineering Research.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0e905aee3c4fcddf11fe0c265dadcef7
https://doi.org/10.1063/5.0132289
https://doi.org/10.1063/5.0132289
Publikováno v:
Warta Ardhia: Jurnal Perhubungan Udara, Vol 44, Iss 2, Pp 93-98 (2019)
Sehubungan dengan kestabilan dan pengendalian dari pesawat WISE L8, maka perlu didefinisikan bahwa wahana terbang tersebut sudah memenuhi beberapa persyaratan prestasi terbang agar dapat kontiniu take off dari permukaan air. Pada paper ini diperlihat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::23234a22bade651908804bd4e2834c81
http://www.wartaardhia.com/index.php/wartaardhia/article/view/331
http://www.wartaardhia.com/index.php/wartaardhia/article/view/331
Autor:
Sayuti Syamsuar
Publikováno v:
Warta Ardhia: Jurnal Perhubungan Udara, Vol 44, Iss 1, Pp 57-64 (2018)
The Hydrodynamic and Aerodynamic Characteristics of WISE L8 During Hydro Planing and Airborne Base On CFD: This paper explains why the computational fluid dynamics is used on the model 3-D CATIA of Wing in Surface Effect craft WISE Lippisch configura
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0ea390c82ad103dae9cfb149741ac821
https://doi.org/10.25104/wa.v44i1.329.57-64
https://doi.org/10.25104/wa.v44i1.329.57-64
Autor:
Sayuti Syamsuar
Publikováno v:
Warta Ardhia: Jurnal Perhubungan Udara, Vol 43, Iss 2, Pp 141-148 (2017)
This paper provides an overview of the design of adaptive flight control system of wing in surface effect craft Lippisch configuration 8 passengers capacity during cruise in the low speed and low altitude. The control system will be used the control
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c520e19c3d4c9b528b0c226d9f86e034
https://doi.org/10.25104/wa.v43i2.295.141-148
https://doi.org/10.25104/wa.v43i2.295.141-148
Publikováno v:
Warta Ardhia: Jurnal Perhubungan Udara, Vol 43, Iss 2, Pp 117-124 (2017)
The surface effect flight adaptive flight control system design has been analyzed by root locus method and gain scheduling on Tune PID controller in the low speed, V and surface effect altitude, h. The several parameters in the Single Input Single Ou
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6bc22e7507bd2f6c35c732f8e4327ae9
http://www.wartaardhia.com/index.php/wartaardhia/article/view/303
http://www.wartaardhia.com/index.php/wartaardhia/article/view/303
Autor:
Sayuti Syamsuar
Publikováno v:
Warta Ardhia: Jurnal Perhubungan Udara, Vol 42, Iss 1, Pp 1-6 (2017)
Pesawat Wing In Surface Effect A2B tipe B konfigurasi Lippisch mempunyai hambatan air yang cukup besar dibandingkan tenaga mesin saat hydroplaning. Makalah ini berisikan bagian dari analisis dalam perancangan untuk mengetahui karakteristik aerodinami
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::59c5dfb8c96e48501c30997f565a0cea
https://doi.org/10.25104/wa.v42i1.294.1-6
https://doi.org/10.25104/wa.v42i1.294.1-6
Publikováno v:
Warta Ardhia: Jurnal Perhubungan Udara, Vol 42, Iss 3, Pp 123-138 (2017)
Fenomena flutter merupakan salah satu fenomena yang kritis dan dapat membahayakan pesawat. Ketika, pesawat terbang semakin cepat dan mencapai kecepatan flutter, maka akan terjadi ketidakstabilan struktur. Oleh sebab itu, untuk menjamin keselamatan Pi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::379402ca53fd3c86a687d3d297d19123
https://doi.org/10.25104/wa.v42i3.242.123-138
https://doi.org/10.25104/wa.v42i3.242.123-138
Publikováno v:
Warta Ardhia: Jurnal Perhubungan Udara, Vol 42, Iss 4, Pp 165-172 (2017)
Fenomena flutter akan terjadi apabila ada gaya dan momen aerodinamika yang berinteraksi berlebihan di permukaan sayap di dalam terowongan angin atau pesawat sesungguhnya. Sayap akan bergetar dan berosilasi bertambah besar menuju ke keadaan tidak stab
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e993a812049aba395d8bddfd5e7d639e
http://www.wartaardhia.com/index.php/wartaardhia/article/view/246
http://www.wartaardhia.com/index.php/wartaardhia/article/view/246
Autor:
Sayuti Syamsuar
Publikováno v:
Warta Ardhia: Jurnal Perhubungan Udara, Vol 41, Iss 3, Pp 139-146 (2017)
The paper presents an analysis of the flight performance and stability and control of a Flying Boat remote control model on the ground effect altitude. It begins with a three dimensional measurement of a Flying Boat remote control model by using a la
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::db4eda5a8c8b22079afc42181535944e
https://doi.org/10.25104/wa.v41i3.151.139-146
https://doi.org/10.25104/wa.v41i3.151.139-146