Descriptive Twin Floater98 and Aircraft in Wind Tunnel Test

Name: Descriptive Twin Floater98 and Aircraft in Wind Tunnel Test
Creator: Karyawan Karyawan
Published: 2024-04-23T11:12:34.990Z
Keywords: Aerodynamics

Karyawan, Karyawan; Syamsuar, Sayuti; Suwasono, Bagiyo; Widyawasta, Widyawasta; Basuki, Agus; Wijiatmoko, Gunawan; Kooshartoyo, Meedy; Muflih, Muhamad; Mahardiani, Sulma; Widyawati, Gusty; Anisa Rachma, Shifana; Novianti, Hetty; Zuhdi Pane, Ivransa; Tauviqirrahman, Muhammad; Yohana, Eflita

doi:10.17632/pyp993dc7t.4

Descriptive Twin Floater98 and Aircraft in Wind Tunnel Test

Published: 23 April 2024| Version 4 | DOI: 10.17632/pyp993dc7t.4

Contributors:

Karyawan Karyawan, Sayuti Syamsuar,

, Widyawasta Widyawasta, Agus Basuki, Gunawan Wijiatmoko, Meedy Kooshartoyo, Muhamad Muflih, Sulma Mahardiani, Gusty Widyawati, Shifana Anisa Rachma, Hetty Novianti, Ivransa Zuhdi Pane, Muhammad Tauviqirrahman, Eflita Yohana

Description

The aerodynamic testing of the N219A aircraft test model with a catamaran floater with a scale of 1:6.3 was carried out in the wind tunnel test section of the Indonesian Low Speed Tunnel (ILST) in 2023. There were 2 measurements including forces and moments with various configurations and variations in deflection angles of the control surface and flaps. The wind speed in the test was 65 m/s. Measurement data is corrected including weight correction, zero correction, blockage correction, tare correction, and wall interference.

Descriptive Twin Floater98 and Aircraft in Wind Tunnel Test

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