Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds
Yıl: 2022 Cilt: 8 Sayı: 4 Sayfa Aralığı: 600 - 613 Metin Dili: İngilizce DOI: 10.28979/jarnas.1069147 İndeks Tarihi: 22-12-2022
Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds
Öz: An aerodynamic technique to calculating lift and drag coefficients is one of the required instruments in the wing design process. During the last decades, several tools and software have been developed according to aero-dynamics and numerical methods. Nowadays, aeronautical architecture requires many calculations. Today’s techno-logists use a variety of simulation techniques to avoid a expensive model testing. This paper explains how wing profiles can be modelled using ANSYS Fluent and tested by low-speed tests considering experimental literature re-sults. With the selected wing profile, the geometry is shaped in two dimensions and designed in three dimensions. Computational fluid dynamics (CFD) was adopted as the method for studying wing profiles. Wing profiles created at 0 to 20-degree attack angles are calculated in the simulation area equal to the actual wind tunnel scale, and equations are solved using the RNG k-Epsilon turbulence model. The process of developing the grids was realized with Ansys Mesher software. The solution stage and the result show operations were carried out with the CFD Post software. The study of the low velocity and high transport wing profiles, the drag coefficient, the lift coefficient, and the effect on the lift-drag ratio were studied using a numerical procedure. After determining the high efficiency of wing profi-les, production of a selected profile began with a static examination.
Anahtar Kelime: Belge Türü: Makale Makale Türü: Araştırma Makalesi Erişim Türü: Erişime Açık
- Anderson, J. D. (1999). Aircraft Performance and Design, Boston, WCB/McGraw-Hill. Retrieved from: https://www.academia.edu/40606141/AIRCRAFT_PERFORMANCE_AND_DESIGN
- Anderson, J. D. (2001). Introduction to Flight, McGraw-Hill, New York. Retrieved from: http://ae.sharif.edu/~iae/Download/Introduction%20to%20flight.pdf
- Aviation Outlook. (2021). Retrieved from: https://www.compositesworld.com/articles/aviation-outlook-fuel- pricing-ignites-demand-for-composites-in-commercial-transports.
- Chitte, P., Jadhav, P. K., & Bansode, S. S. (2013). Statistic and Dynamic Analysis of Typical Wing Structure of Aircraft Using Nastran. International Journal of Application or Innovation in Engineering & Management, ISSN: 2319-4847.
- Choubey, G., Suneetha, L., Pandey, K. M. (2018). Composite Materials Used in Scramjet- A Review. Materials Today: Proceedings, 5, pp. 1321-1326. doi: https://doi.org/10.1016/j.matpr.2017.11.217
- Davies, P., Choqueuse, D., & Devaux, H. (2012). Failure of Polymer Matrix Composites in Marine and Off- shore Applications. Failure Mechanisms in Polymer Matrix Composites. 1st ed., Woodhead Publishing, Cambridge, pp. 300-336. ISBN-13: 978-1845697501.
- Delogu, M., Zanchi, L., Dattilo, C.A., Pierini, M. (2017). Innovative Composites and Hybrid Materials for Electric Vehicles Lightweight Design in a Sustainability Perspective. Materials Today Communications, 13, pp. 192-209. doi: https://doi.org/10.1016/j.mtcomm.2017.09.012
- Epoksi hexion. (2021). Retrieved from: https://www.dostkimya.com/tr/urunler/epoksi-sistemler/laminasyon- epoksi-hexion-mgs-l285-sistemi
- Fertis, D. G. (1994). New Airfoil Design Concept with Improved Aerodynamic Characteristics. Journal of Aerospace Engineering, 7(3), pp. 328-339. doi: https://doi.org/10.1061/(ASCE)0893- 1321(1994)7:3(328)
- Henne, P. A. (1990). Applied Computational Aerodynamics, Washington DC, American Institute of Aeronautics and Astronautics. ISBN: 093040369X 9780930403690
- Jaroslaw, S., Raphael, T. (1996). Multidisciplinary Aerospace Design Optimization: Survey of Recent Developments, Structural Optimization, 14, pp. 1-23. doi:10.1007/BF01197554
- Jones, W. P., Launder, B. E. (1972). The Prediction of Laminarization with a Two-Equation Model of Turbulence. International Journal of Heat and Mass Transfer, vol. 15, pp. 301-314. doi: https://doi.org/10.1016/0017-9310(72)90076-2
- Jony, H. N., Hossain, S., Raiyan, F. M., Akanda, U. N. M. (2014). A Comparative Flow Analysis of Naca6409 and Naca4412 Aerofoil. International Journal of Research in Engineering and Technology, 03(10), pp. 342–350.
- Kanesan, G., Mansor, S., Abdul-Latif, A. (2014). Validation of UAV Wing Structural Model for Finite Element Analysis. J Teknol, 71, pp. 1-5. doi:10.11113/jt.v71.3710
- Karthigeyan, P., Raja, M. S., Hariharan, R., Karthikeyan, R., Prakash, S. (2017). Performance Evaluation of Composite Material for Aircraft Industries. Materials Today: Proceedings, 4, pp.3263-3269. doi: https://doi.org/10.1016/j.matpr.2017.02.212
- Kumara, S. M., Raghavendra, K., Venkataswamy, A. M., Ramachandra, H. V. (2012). Fractographic Analysis of Tensile Failures of Aerospace Grade Composites. Material Research, 15(6), 990-997. doi: https://doi.org/10.1590/S1516-14392012005000141
- Launder, B. E., Sharma, B. I. (1974). Application of the Energy Dissipation Model of Turbulence to the Calculation of Flow Near a Spinning Disc. Letters in Heat and Mass Transfer, vol. 1, no. 2, pp. 131- 138. doi: https://doi.org/10.1016/0094-4548(74)90150-7
- Lee, J. Y., Yan, J. A., Chua, C. K. (2017), Fundamentals, and applications of 3D printing for novel materials. Applied Materials Today, 7, pp. 120-133. doi: https://doi.org/10.1016/j.apmt.2017.02.004
- Meganathan, V. (2014). Aircraft Design Project-I: Heavy Business Jet. Retrieved from: https://www.researchgate.net/publication/263850415_AIRCRAFT_DESIGN_PROJECT_- I_Heavy_Business_Jet
- Onour, H. K., Jahangiri, M., Sedaghat, A. (2011). Theoretical Aerodynamic Analysis of Six Airfoils for Use on Small Wind Turbines, Proceedings of the 1st International Conference on Emerging Trends in Energy Conservation – ETEC, Tehran, Iran, 20-21 November.
- Parashar, H. (2015). Calculation of Aerodynamic Characteristics of NACA 2415, 23012, 23015 Airfoils Using Computational Fluid Dynamics (CFD). International Journal of Science, Engineering and Technology Research, 4(3), pp. 610–614. Retrieved from: http://ijsetr.org/wpcontent/uploads/2015/03/IJSETR- VOL-4- ISSUE-3-610-614.pdf
- Sadraey, M. (2013). Aircraft Design: A Systems Engineering Approach, 1st ed., Wiley, New Hampshire. ISBN: 978-1-119-95340-1.
- Schmid Fuertes, T.A., Kruse, T., Korwien, T., & Geistbeck, M. (2015). Bonding of CFRP Primary Aerospace Structures - Discussion of the Certification Boundary Conditions and Related Technology Fields Addressing the Needs for Development. Composite Interfaces, 22(8), pp. 795-808. doi: https://doi.org/10.1080/09276440.2015.1077048
- Schwartz, M. (1992). Composite Materials Handbook, 2nd ed., McGraw-Hill, New York. ISBN: 0070558191 9780070558199
- Shama, R. N., Simha, T. G. A., Rao K, P., Kumar, R. G. V. V. (2020), Carbon Composites Are Becoming Competitive and Cost Effective, Infosys Limited, Retrieved from: https://www.infosys.com/engineering-services/white-papers/Documents/carbon-composites-cost- effective.pdf
- Sharma, S. (2016). An Aerodynamic Comparative Analysis of Airfoils for Low-Speed Aircrafts, International Journal of Engineering Research, V5 (11), pp. 525–529. doi:10.17577/IJERTV5IS110361
- Sobieczky, H. (1999). Parametric Airfoils and Wings, In: Fujii K., Dulikravich G.S., Recent Development of Aerodynamic Design Methodologies, Notes on Numerical Fluid Mechanics (NNFM), vol 65, Vieweg+Teubner Verlag, doi:10.1007/978-3-322-89952-1_4
- Stollery, J. L. (2017). Aerodynamics, Aeronautics and Flight Mechanics, In Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 211, doi: https://doi.org/10.1177/095441009721100102
- Syamsuar, S., Djatmiko, E. B., Erwandi, E., Mujahid, A. S., Subchan, S. (2016). The Hydroplaning Simulation of Flying Boat Remote Control Model, Jurnal Teknologi, 78(6), pp. 191–197, doi: https://doi.org/10.11113/jt.v78.4267
- Wu, W., Sun, Q., Luo, S., Sun, M., Chen, Z., & Sun, H. (2018). Accurate calculation of aerodynamic coefficients of parafoil airdrop system based on computational fluid dynamic. International Journal of Advanced Robotic Systems, 15(2). doi: https://doi.org/10.1177/1729881418766190
- Yadav, S., Gangwar, S., Singh, S. (2017). Micro/Nano Reinforced Filled Metal Alloy Composites: A Review Over Current Development in Aerospace and Automobile Applications. Materials Today: Proceedings, 4, pp. 5571-5582. doi: https://doi.org/10.1016/j.matpr.2017.06.014
- Yongchang, Y., Zhang, S., Li, H., Wang, X., Tang, Y. (2017). Modal and Harmonic Response Analysis of Key Components of Ditch Device Based on ANSYS, Procedia Engineering, 174, pp. 956–64, doi: https://doi.org/10.1016/j.proeng.2017.01.247
- См, Егер. (1986). Основы автоматизированного проектирования самолетов.Машиностроение, pp. 232, Москва. Retrieved from: https://www.dissercat.com/content/avtomatizatsiya-dokumentirovaniya- protsessa-formirovaniya-otseka-magistralnogo-samoleta
| APA | ÜRGÜN S, GÖKDEMİR M, Fidan S (2022). Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds. , 600 - 613. 10.28979/jarnas.1069147 |
| Chicago | ÜRGÜN Satılmış,GÖKDEMİR Mert,Fidan Sinan Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds. (2022): 600 - 613. 10.28979/jarnas.1069147 |
| MLA | ÜRGÜN Satılmış,GÖKDEMİR Mert,Fidan Sinan Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds. , 2022, ss.600 - 613. 10.28979/jarnas.1069147 |
| AMA | ÜRGÜN S,GÖKDEMİR M,Fidan S Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds. . 2022; 600 - 613. 10.28979/jarnas.1069147 |
| Vancouver | ÜRGÜN S,GÖKDEMİR M,Fidan S Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds. . 2022; 600 - 613. 10.28979/jarnas.1069147 |
| IEEE | ÜRGÜN S,GÖKDEMİR M,Fidan S "Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds." , ss.600 - 613, 2022. 10.28979/jarnas.1069147 |
| ISNAD | ÜRGÜN, Satılmış vd. "Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds". (2022), 600-613. https://doi.org/10.28979/jarnas.1069147 |
| APA | ÜRGÜN S, GÖKDEMİR M, Fidan S (2022). Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds. Journal of advanced research in natural and applied sciences (Online), 8(4), 600 - 613. 10.28979/jarnas.1069147 |
| Chicago | ÜRGÜN Satılmış,GÖKDEMİR Mert,Fidan Sinan Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds. Journal of advanced research in natural and applied sciences (Online) 8, no.4 (2022): 600 - 613. 10.28979/jarnas.1069147 |
| MLA | ÜRGÜN Satılmış,GÖKDEMİR Mert,Fidan Sinan Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds. Journal of advanced research in natural and applied sciences (Online), vol.8, no.4, 2022, ss.600 - 613. 10.28979/jarnas.1069147 |
| AMA | ÜRGÜN S,GÖKDEMİR M,Fidan S Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds. Journal of advanced research in natural and applied sciences (Online). 2022; 8(4): 600 - 613. 10.28979/jarnas.1069147 |
| Vancouver | ÜRGÜN S,GÖKDEMİR M,Fidan S Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds. Journal of advanced research in natural and applied sciences (Online). 2022; 8(4): 600 - 613. 10.28979/jarnas.1069147 |
| IEEE | ÜRGÜN S,GÖKDEMİR M,Fidan S "Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds." Journal of advanced research in natural and applied sciences (Online), 8, ss.600 - 613, 2022. 10.28979/jarnas.1069147 |
| ISNAD | ÜRGÜN, Satılmış vd. "Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds". Journal of advanced research in natural and applied sciences (Online) 8/4 (2022), 600-613. https://doi.org/10.28979/jarnas.1069147 |
