Dataset of the twin floater of amphibian aircraft in wind tunnel test
It is well known that seaplanes have twin floaters. Therefore, it is necessary to conduct a wind tunnel test that aims to determine the performance of twin floaters paired on a mock aircraft model. The twin floaters use the same scale as the mock aircraft, which is 1:6.3 with a length of 1555 mm and a distance between floaters of 668.8 mm or S/L of 0.43. The test plan uses a speed of 65 m s<sup>-1</sup> and a Reynolds number 1.5 times the model configuration with flap angle variations of 0°, 10°, 18°, 30°, and 40°. The final test results showed that tabulations and graphs of lift coefficient (C<sub>L</sub>), drag coefficient (C<sub>D</sub>), and pitching moment coefficient (C<sub>M</sub>) with angle of attack (α) variations of -10° to 16°.
Authors
- Mohammad Tauviqirrahman (ORCID: https://orcid.org/0000-0003-2694-4184)
- Bagiyo Suwasono (ORCID: https://orcid.org/0000-0002-5181-4106)
- Supartono Supartono
- Karyawan Karyawan
- Eflita Yohana (ORCID: https://orcid.org/0000-0003-2408-2912)
- Ivransa Zuhdi Pane
- Aam Muharam (ORCID: https://orcid.org/0000-0001-8803-7999)
- Sayuti Syamsuar
- Widyawasta
- Ismoyo Haryanto
Institutions
- Diponegoro University (ID)
- Dynamic Research (United States) (US)
- Universitas Hang Tuah (ID)
- National Nuclear Energy Agency of Indonesia (ID)
Publication Details
- Journal
- Data in Brief
- Published
- 2024-10-11
- DOI
- https://doi.org/10.1016/j.dib.2024.111008
- Primary Topic
- Aerospace and Aviation Technology
- Type
- article
- Field-Weighted Citation Impact
- 0.00
Funders
- Badan Riset dan Inovasi Nasional
- Universitas Diponegoro
- Lembaga Pengelola Dana Pendidikan
- Kementerian Keuangan Republik Indonesia