Descriptive Twin Floater98 and Aircraft in Wind Tunnel Test

Name: Descriptive Twin Floater98 and Aircraft in Wind Tunnel Test
Creator: Karyawan Karyawan
Published: 2024-04-16T13:12:13.701Z
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.3

Descriptive Twin Floater98 and Aircraft in Wind Tunnel Test

Published: 16 April 2024| Version 3 | DOI: 10.17632/pyp993dc7t.3

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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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