Main Article Content
Abstract
Information on weather conditions is needed to support flight safety, especially in the process take-off. One of the required weather information is wind data, wind direction and wind speed. One of the wind components is the tailwind(wind from behind). In the small airports it can only be visited by aircraft such as ATR72 and its kind, due to the limited availability of runways and currently many of these airports are still using landing and take-off in the direction of thewind. This can result in a lack of lift during take-off during the tailwind conditions. To prevent this from happening, there is a reduction in the capacity of the aircraft. The purpose of this study was to analyze the performance of the ATR72 aircraft during take-off with tailwind conditions. By calculating the takeoff under normal conditions on the ATR72 aircraft then varying the tailwind speed. The results obtained are the value of the ground roll distance (????????) and the reduction in aircraft weight (????) at the time of tailwind. a speed tailwind of 0 or normal, obtained a distance of ground roll 849 m, take-off weight of 20948 kg, reduction in aircraft weight of 0. Speed tailwind of 5 kts, distance of ground roll 773 m, take-off weight of 20333 kg, reduction in aircraft weight of 615 kg, while speed of tailwind 10 kts obtained distance of ground roll 697 m, take-off weight of 19308 kg, reduction in aircraft weight of 1640 kg, and speedtailwind of 15 kts, distance of ground roll 621 m, take-off weight of 18225 kg, was obtained. reduction in aircraft weight by 2723 kg.
Keywords
ATR72
ground roll
reduction aircraft weight
tailwind
take-off
Article Details
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.
How to Cite
Fahreza Andreanto, D. ., Arifin, M. ., Franciscus, F. ., & Endarti, E. (2023). Analisis Performa Takeoff Pada Pesawat ATR 72 Dalam Pengaruh Tailwind. Jurnal Teknologi Kedirgantaraan, 8(2). https://doi.org/10.35894/jtk.v8i2.86 (Original work published August 31, 2023)
References
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Ruijgrok, G.J.J., 1994, Elements of Airplane Performance, Faculty of Aerospace Engineering, Netherlands: Delft University of Technology.
Nita, Florentina Mihaela. 2008. Aircraft Design Studies Based on the ATR 72, Department of Automotive and Aeronautical Engineering, Germany: Hamburg University.
Federal Aviation Administration, 2016, Weight and Balance Handbook US: Department of Transportation.
Fadholi, Akhmad, 2013, Analisis Komponen Angin Landas Pacu (Runway) Bandara Depati Amir Pangkal pinang, Jurnal Stasiun Meteorologi Pangkal pinang, No. 2, Vol. 13, 45 – 53.
Anderson, J.D. 1998, Aircraft Performance and Design, Mcgraw-Hill Education.
Roskam, Jan, 1985, Airplane Design Part 1: Preliminary Sizing of Airplanes, Ackers Distinguished Professor of Aerospace Engineering, USA: The University of Kansas.
Kristanto, Philip, 2020, Fisika Dasar – Teori, Soal, dan Penyelesaian, Yogyakarta: ANDI.
ATR CM Marketing, 2015 https://skybrary.aero/bookshelf/books/3696.pdf diakses pada tanggal 16 Desember 2020.
Departemen Perhubungan, 2019, http://hubud.dephub.go.id/website/BandaraDetail.php?id=109 diakses pada tanggal 16 Desember 2020
References
Ruijgrok, G.J.J., 1994, Elements of Airplane Performance, Faculty of Aerospace Engineering, Netherlands: Delft University of Technology.
Nita, Florentina Mihaela. 2008. Aircraft Design Studies Based on the ATR 72, Department of Automotive and Aeronautical Engineering, Germany: Hamburg University.
Federal Aviation Administration, 2016, Weight and Balance Handbook US: Department of Transportation.
Fadholi, Akhmad, 2013, Analisis Komponen Angin Landas Pacu (Runway) Bandara Depati Amir Pangkal pinang, Jurnal Stasiun Meteorologi Pangkal pinang, No. 2, Vol. 13, 45 – 53.
Anderson, J.D. 1998, Aircraft Performance and Design, Mcgraw-Hill Education.
Roskam, Jan, 1985, Airplane Design Part 1: Preliminary Sizing of Airplanes, Ackers Distinguished Professor of Aerospace Engineering, USA: The University of Kansas.
Kristanto, Philip, 2020, Fisika Dasar – Teori, Soal, dan Penyelesaian, Yogyakarta: ANDI.
ATR CM Marketing, 2015 https://skybrary.aero/bookshelf/books/3696.pdf diakses pada tanggal 16 Desember 2020.
Departemen Perhubungan, 2019, http://hubud.dephub.go.id/website/BandaraDetail.php?id=109 diakses pada tanggal 16 Desember 2020
Nita, Florentina Mihaela. 2008. Aircraft Design Studies Based on the ATR 72, Department of Automotive and Aeronautical Engineering, Germany: Hamburg University.
Federal Aviation Administration, 2016, Weight and Balance Handbook US: Department of Transportation.
Fadholi, Akhmad, 2013, Analisis Komponen Angin Landas Pacu (Runway) Bandara Depati Amir Pangkal pinang, Jurnal Stasiun Meteorologi Pangkal pinang, No. 2, Vol. 13, 45 – 53.
Anderson, J.D. 1998, Aircraft Performance and Design, Mcgraw-Hill Education.
Roskam, Jan, 1985, Airplane Design Part 1: Preliminary Sizing of Airplanes, Ackers Distinguished Professor of Aerospace Engineering, USA: The University of Kansas.
Kristanto, Philip, 2020, Fisika Dasar – Teori, Soal, dan Penyelesaian, Yogyakarta: ANDI.
ATR CM Marketing, 2015 https://skybrary.aero/bookshelf/books/3696.pdf diakses pada tanggal 16 Desember 2020.
Departemen Perhubungan, 2019, http://hubud.dephub.go.id/website/BandaraDetail.php?id=109 diakses pada tanggal 16 Desember 2020