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Abstract
Aerodynamic characteristics can be known by using computational Fluid Dynamics(CFD) methods. This study analyzes the pressure distribution andvelocity of air flow on FuselageB737-9 MAX using the Computational Fluid Dynamics (CFD) method with variations in attackangles of 0o, 15o, 30oand 45o. The results obtained are at 0oattack angle, 15othe difference inspeed and pressure is not too significant or normal, while at the attack angle 30oand 45othedifference in speed and pressure is very significant or abnormal because the air flow at that angleexperiences turbulence around the fuselage.
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References
- Federal Aviation Administration. 2012. Aviation Maintance TechnicianHandbook-airframe. USA : Departmentof Transportationhttps://www.faa.gov/regulations_policies/handbooks_manuals/aviation/phak/media/05_phak_ch3.pdf, diakses pada tanggal 30 Juni 2018
- Boeing Commercial Airplanes, 2018, Configuration Specification Boeing 737-MAX 9, USA
- Boeing 737-MAX 9 Efficiancy, Reliability,Passenger appealhttps://www.boeing.com/commercial/737max/,diakses pada29 Juni 2018
- Anderson, Jhon D, Jr. 1995. Computational Fluida Dynamic (2nded). New York: McGraw
References
Federal Aviation Administration. 2012. Aviation Maintance TechnicianHandbook-airframe. USA : Departmentof Transportationhttps://www.faa.gov/regulations_policies/handbooks_manuals/aviation/phak/media/05_phak_ch3.pdf, diakses pada tanggal 30 Juni 2018
Boeing Commercial Airplanes, 2018, Configuration Specification Boeing 737-MAX 9, USA
Boeing 737-MAX 9 Efficiancy, Reliability,Passenger appealhttps://www.boeing.com/commercial/737max/,diakses pada29 Juni 2018
Anderson, Jhon D, Jr. 1995. Computational Fluida Dynamic (2nded). New York: McGraw