ANALISIS PERFORMA AERODINAMIKA NACA 642415 DUA DIMENSI MENGGUNAKAN APLIKASI XFLR5 SEBAGAI BASELINE PENELITIAN
Abstract
Baseline penelitian diperlukan untuk tindak lanjut penelitian selanjutnya. Selain dari eksperimen, penggunaan simulasi numerik sederhana dapat menjadi pembanding secara singkat performa aerodinamika dari airfoil maupun sayap pesawat terbang dan UAV. Penelitian ini menunjukkan peforma aerodinamika NACA 642415 menggunakan aplikasi XFLR5 dengan sudut serang α = 0o, 2o, 4o, 6o, 8o, 10o, 12o, 14o, 16o, 18o, dan 20o. XFLR5 dapat menunjukkan secara singkat dan cepat performa aerodinamika dari airfoil dan sayap. Koefisien tekanan yang dihasilkan dapat menunjukkan secara ringkas titik separasi dan titik stall yang terjadi meskipun tidak dapat ditunjukkan secara langsung melalui hasil koefisien lift.
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References
Akhil P Thomas, Nandu S Nair, Abin Jose, & Neethi Madhavan CS. (2023). Design and Analysis of Flexible Wing. ACS Journal for Science and Engineering, 3(1), 42–52. https://doi.org/10.34293/acsjse.v3i1.60
Almallah, S. H., Elnady, A. O., & Okasha Elnady, A. (2023). CFD Analysis of Full Quadcopter. International Journal of Advanced Multidisciplinary Research and Studies, 2(December 2022), 599–604. https://www.researchgate.net/publication/365999969
Ananda, G. K., & Selig, M. S. (2016). Stall/post-stall modeling of the longitudinal characteristics of a general aviation aircraft. AIAA Atmospheric Flight Mechanics Conference, 2016-Janua(June 2016), 27. https://doi.org/10.2514/6.2016-3541
Anderson, J. D. (2012). Fundamentals of Aerodynamics — Fifth edition. In The Aeronautical Journal (Vol. 116, Issue 1176). https://doi.org/10.1017/S000192400000676X
Aprovitola, A., Dyblenko, O., Pezzella, G., & Viviani, A. (2022). Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions. Aerospace, 9(8). https://doi.org/10.3390/aerospace9080411
Chinnappa, V., & Srinivas, G. (2023). Numerical investigation of Aerodynamic Characteristics of NACA 23112 Using Passive Flow Control Technique–Gurney Flaps. Cogent Engineering, 10(1), 1–19. https://doi.org/10.1080/23311916.2023.2222566
Communier, D., Salinas, M. F., Carranza Moyao, O., & Botez, R. M. (2015). Aero Structural Modeling of a Wing using CATIA V5 and XFLR5 Software and Experimental Validation using the Price- Païdoussis Wing Tunnel. August. https://doi.org/10.2514/6.2015-2558
Fernando, V. N., & Mudunkotuwa, D. Y. (2021). Bio-Inspired Aircraft Wing Modification Analysis in ANSYS Fluent. 2021 10th International Conference on Information and Automation for Sustainability, ICIAfS 2021, August, 316–321. https://doi.org/10.1109/ICIAfS52090.2021.9605821
Gudmundsson, S. (2013). General Aviation Aircraft Design : Applied Methods (First edit). Butterworth-Heinemann is an imprint of Elsevier.
Guzelbey, İ. H., Eraslan, Y., & Dogru, M. H. (2018). Numerical Investigation of Different Airfoils at Low Reynolds Number in terms of Aerodynamic Performance of Sailplanes by using XFLR5. Karadeniz Fen Bilimleri Dergisi, 8(1), 47–65. https://doi.org/10.31466/kfbd.423932
Hariyadi, S. S. P., Sutardi, & Widodo, W. A. (2018). Drag reduction analysis of wing airfoil E562 with forward wingtip fence at cant angle variations of 75°and 90°. AIP Conference Proceedings, 2001. https://doi.org/10.1063/1.5049994
Hariyadi, S., Sutardi, S., Widodo, W. A., & Junipitoyo, B. (2019). Numerical Study of the Wingtip Fence on the Wing Airfoil E562 with Fence Height Variations. October, 16–17.
Hızalan, O., Topçam, A. M., Özsunar, S., Doğan, S., & Ödemiş, A. (2023). Vibratory and Static Analysis of AIRBUS A300 Airplane Wing Model using ANSYS Workbench. IES 22 International Engineering Symposium, January, 11.
Houghton, E. L., Carpenter, P. W., Collicott, S. H., & Valentine, D. T. (2013). Aerodynamics for Engineering Students. Butterworth-Heinemann is an imprint of Elsevier. http://search.ebscohost.com/login.aspx?direct=true&db=cat00164a&AN=cran.579071&site=eds-live%5Cnhttp://www.cranfield.eblib.com/patron/FullRecord.aspx?p=879862
Inamul Hasan M, Ramanan G, & Manishankar V. (2022). Study and Comparison Analysis of Conventional Light Weight UAV Airfoils using XFLR Analysis. ACS Journal for Science and Engineering, 2(1), 1–9. https://doi.org/10.34293/acsjse.v2i1.22
Islas-Narvaez, E. A., Ituna-Yudonago, J. F., Ramos-Velasco, L. E., Vega-Navarrete, M. A., & Garcia-Salazar, O. (2023). Design and Determination of Aerodynamic Coefficients of a Tail-Sitter Aircraft by Means of CFD Numerical Simulation. Machines, 11(1), 1–24. https://doi.org/10.3390/machines11010017
Ismeal, I. J., Bakirci, M., & Jweeg, M. J. (2024). An Optimum Design of a Subsonic Aircraft Wing due to the Aerodynamic Loading. Hindawi The Scientifc World Journal, 2024, 13.
Kakade, S., Chikkala, D., Reghunath, K., & Seeni, A. (2022). Aerodynamic Analysis and Optimization of Wings for the Jain University Sailplane Using XFLR5. ECS Transactions, 107(1), 493–513. https://doi.org/10.1149/10701.0493ecst
Kusuma, Y. F., Defianti, H., & Syamsuar, S. (2023). The Effect of Adding Floaters to Airplane Models on Aerodynamic Characteristics Using Computational Fluid Dynamics Methods. AIP Conference Proceedings, 2941(1). https://doi.org/10.1063/5.0181446
Lesalli, P. V., & Cahyono, M. A. (2020). Longitudinal Static Stability Analysis with Wing Swept Angle Variation Of UAV Flying Wing Surveilance Adelaar 2 Use Software XFLR 5. Conference SENATIK STT Adisutjipto Yogyakarta, 6, 35–42. https://doi.org/10.28989/senatik.v6i0.402
Prasetyo, F. K. P. B., Marausna, G., & Jayadi, F. (2023). Analisis Bentuk Wing Uav Strike 50 dengan Menggunakan Software Xflr5 dan Datcom. JETISH: Journal of Education Technology Information Social Sciences and Health, 1(1), 1–6. https://doi.org/10.57235/jetish.v1i1.26
Putro, S. H. S., Sutardi, & Widodo, W. A. (2019). Numerical study of three-dimensional flow characteristics around the wing airfoil E562 with forward and rearward wingtip fence. 020017. https://doi.org/10.1063/1.5138272
Rudresh, M., Sudhagara Rajan, S., Prashanth, K. P., Vasist, A. S., Dhaduk, D., Deshmukh, S., & Sahoo, S. (2023). Design and Development of a Flying Wing Reconnaissance UAV. Journal of Engineering Science and Technology, 18(5), 2615–2630.
Setyo Hariyadi, S. P., Sutardi, & Widodo, W. A. (2018). Numerical study of flow characteristics around wing airfoil Eppler 562 with variations of rearward wingtip fence. AIP Conference Proceedings, 1983. https://doi.org/10.1063/1.5046207
Setyo Hariyadi, S. P., Sutardi, Widodo, W. A., & Mustaghfirin, M. A. (2018). Aerodynamics Analysis of the Wingtip Fence Effect on UAV Wing. International Review of Mechanical Engineering, 12(10), 837–846. https://doi.org/10.15866/ireme.v12i10.15517
Setyo Hariyadi, S. P., Sutardi, Widodo, W. A., & Rachmadiyan, A. (2018). Numerical simulation of airfoil Eppler 562 with variations of whitcomb wingtip devices. AIP Conference Proceedings, 1983. https://doi.org/10.1063/1.5046199
Yang, M., Wang, S., Hu, K., & Liu, T. (2023). Wing Optimization Design Based on Composite Global Hawk Unmanned Aerial Vehicle. Journal of Physics: Conference Series, 2557(1). https://doi.org/10.1088/1742-6596/2557/1/012087
Almallah, S. H., Elnady, A. O., & Okasha Elnady, A. (2023). CFD Analysis of Full Quadcopter. International Journal of Advanced Multidisciplinary Research and Studies, 2(December 2022), 599–604. https://www.researchgate.net/publication/365999969
Ananda, G. K., & Selig, M. S. (2016). Stall/post-stall modeling of the longitudinal characteristics of a general aviation aircraft. AIAA Atmospheric Flight Mechanics Conference, 2016-Janua(June 2016), 27. https://doi.org/10.2514/6.2016-3541
Anderson, J. D. (2012). Fundamentals of Aerodynamics — Fifth edition. In The Aeronautical Journal (Vol. 116, Issue 1176). https://doi.org/10.1017/S000192400000676X
Aprovitola, A., Dyblenko, O., Pezzella, G., & Viviani, A. (2022). Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions. Aerospace, 9(8). https://doi.org/10.3390/aerospace9080411
Chinnappa, V., & Srinivas, G. (2023). Numerical investigation of Aerodynamic Characteristics of NACA 23112 Using Passive Flow Control Technique–Gurney Flaps. Cogent Engineering, 10(1), 1–19. https://doi.org/10.1080/23311916.2023.2222566
Communier, D., Salinas, M. F., Carranza Moyao, O., & Botez, R. M. (2015). Aero Structural Modeling of a Wing using CATIA V5 and XFLR5 Software and Experimental Validation using the Price- Païdoussis Wing Tunnel. August. https://doi.org/10.2514/6.2015-2558
Fernando, V. N., & Mudunkotuwa, D. Y. (2021). Bio-Inspired Aircraft Wing Modification Analysis in ANSYS Fluent. 2021 10th International Conference on Information and Automation for Sustainability, ICIAfS 2021, August, 316–321. https://doi.org/10.1109/ICIAfS52090.2021.9605821
Gudmundsson, S. (2013). General Aviation Aircraft Design : Applied Methods (First edit). Butterworth-Heinemann is an imprint of Elsevier.
Guzelbey, İ. H., Eraslan, Y., & Dogru, M. H. (2018). Numerical Investigation of Different Airfoils at Low Reynolds Number in terms of Aerodynamic Performance of Sailplanes by using XFLR5. Karadeniz Fen Bilimleri Dergisi, 8(1), 47–65. https://doi.org/10.31466/kfbd.423932
Hariyadi, S. S. P., Sutardi, & Widodo, W. A. (2018). Drag reduction analysis of wing airfoil E562 with forward wingtip fence at cant angle variations of 75°and 90°. AIP Conference Proceedings, 2001. https://doi.org/10.1063/1.5049994
Hariyadi, S., Sutardi, S., Widodo, W. A., & Junipitoyo, B. (2019). Numerical Study of the Wingtip Fence on the Wing Airfoil E562 with Fence Height Variations. October, 16–17.
Hızalan, O., Topçam, A. M., Özsunar, S., Doğan, S., & Ödemiş, A. (2023). Vibratory and Static Analysis of AIRBUS A300 Airplane Wing Model using ANSYS Workbench. IES 22 International Engineering Symposium, January, 11.
Houghton, E. L., Carpenter, P. W., Collicott, S. H., & Valentine, D. T. (2013). Aerodynamics for Engineering Students. Butterworth-Heinemann is an imprint of Elsevier. http://search.ebscohost.com/login.aspx?direct=true&db=cat00164a&AN=cran.579071&site=eds-live%5Cnhttp://www.cranfield.eblib.com/patron/FullRecord.aspx?p=879862
Inamul Hasan M, Ramanan G, & Manishankar V. (2022). Study and Comparison Analysis of Conventional Light Weight UAV Airfoils using XFLR Analysis. ACS Journal for Science and Engineering, 2(1), 1–9. https://doi.org/10.34293/acsjse.v2i1.22
Islas-Narvaez, E. A., Ituna-Yudonago, J. F., Ramos-Velasco, L. E., Vega-Navarrete, M. A., & Garcia-Salazar, O. (2023). Design and Determination of Aerodynamic Coefficients of a Tail-Sitter Aircraft by Means of CFD Numerical Simulation. Machines, 11(1), 1–24. https://doi.org/10.3390/machines11010017
Ismeal, I. J., Bakirci, M., & Jweeg, M. J. (2024). An Optimum Design of a Subsonic Aircraft Wing due to the Aerodynamic Loading. Hindawi The Scientifc World Journal, 2024, 13.
Kakade, S., Chikkala, D., Reghunath, K., & Seeni, A. (2022). Aerodynamic Analysis and Optimization of Wings for the Jain University Sailplane Using XFLR5. ECS Transactions, 107(1), 493–513. https://doi.org/10.1149/10701.0493ecst
Kusuma, Y. F., Defianti, H., & Syamsuar, S. (2023). The Effect of Adding Floaters to Airplane Models on Aerodynamic Characteristics Using Computational Fluid Dynamics Methods. AIP Conference Proceedings, 2941(1). https://doi.org/10.1063/5.0181446
Lesalli, P. V., & Cahyono, M. A. (2020). Longitudinal Static Stability Analysis with Wing Swept Angle Variation Of UAV Flying Wing Surveilance Adelaar 2 Use Software XFLR 5. Conference SENATIK STT Adisutjipto Yogyakarta, 6, 35–42. https://doi.org/10.28989/senatik.v6i0.402
Prasetyo, F. K. P. B., Marausna, G., & Jayadi, F. (2023). Analisis Bentuk Wing Uav Strike 50 dengan Menggunakan Software Xflr5 dan Datcom. JETISH: Journal of Education Technology Information Social Sciences and Health, 1(1), 1–6. https://doi.org/10.57235/jetish.v1i1.26
Putro, S. H. S., Sutardi, & Widodo, W. A. (2019). Numerical study of three-dimensional flow characteristics around the wing airfoil E562 with forward and rearward wingtip fence. 020017. https://doi.org/10.1063/1.5138272
Rudresh, M., Sudhagara Rajan, S., Prashanth, K. P., Vasist, A. S., Dhaduk, D., Deshmukh, S., & Sahoo, S. (2023). Design and Development of a Flying Wing Reconnaissance UAV. Journal of Engineering Science and Technology, 18(5), 2615–2630.
Setyo Hariyadi, S. P., Sutardi, & Widodo, W. A. (2018). Numerical study of flow characteristics around wing airfoil Eppler 562 with variations of rearward wingtip fence. AIP Conference Proceedings, 1983. https://doi.org/10.1063/1.5046207
Setyo Hariyadi, S. P., Sutardi, Widodo, W. A., & Mustaghfirin, M. A. (2018). Aerodynamics Analysis of the Wingtip Fence Effect on UAV Wing. International Review of Mechanical Engineering, 12(10), 837–846. https://doi.org/10.15866/ireme.v12i10.15517
Setyo Hariyadi, S. P., Sutardi, Widodo, W. A., & Rachmadiyan, A. (2018). Numerical simulation of airfoil Eppler 562 with variations of whitcomb wingtip devices. AIP Conference Proceedings, 1983. https://doi.org/10.1063/1.5046199
Yang, M., Wang, S., Hu, K., & Liu, T. (2023). Wing Optimization Design Based on Composite Global Hawk Unmanned Aerial Vehicle. Journal of Physics: Conference Series, 2557(1). https://doi.org/10.1088/1742-6596/2557/1/012087
Published
2024-06-27
How to Cite
1.
Sukahir. ANALISIS PERFORMA AERODINAMIKA NACA 642415 DUA DIMENSI MENGGUNAKAN APLIKASI XFLR5 SEBAGAI BASELINE PENELITIAN. JIA [Internet]. 2024Jun.27 [cited 2024Jul.3];17(01):23-. Available from: https://journal.ppicurug.ac.id/index.php/jurnal-ilmiah-aviasi/article/view/1026
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