Aerodynamic Aspects in the Formation of the Appearance of Mainline Aircraft at the Preliminary Design Stage

Aerodynamic Aspects in the Formation of the Appearance of Mainline Aircraft at the Preliminary Design Stage

  IJETT-book-cover           
  
© 2023 by IJETT Journal
Volume-71 Issue-5
Year of Publication : 2023
Author : Aleksandr Gorbunov, Aleksei Pripadchev, Aleksandr Magdin, Elena Ezerskaya
DOI : 10.14445/22315381/IJETT-V71I5P212

How to Cite?

Aleksandr Gorbunov, Aleksei Pripadchev, Aleksandr Magdin, Elena Ezerskaya, "Aerodynamic Aspects in the Formation of the Appearance of Mainline Aircraft at the Preliminary Design Stage," International Journal of Engineering Trends and Technology, vol. 71, no. 5, pp. 125-131, 2023. Crossref, https://doi.org/10.14445/22315381/IJETT-V71I5P212

Abstract
The study focuses on the improvement of mainland aircraft aerodynamics. The paper presents a study of the mechanism of the formation of induced drag for a finite-span wing. The authors propose a possible option of considering circulation value as a control parameter in the preliminary design of the wings of mainland aircraft equipped with wingtips. The research results may serve as a basis for the conceptual model, mathematical software, and application software implementing the methodology for selecting the composition of rational engineering parameters. The implementation of these findings could lead to increased fuel efficiency, reduced emissions, and overall better performance of mainland aircraft, contributing to a more sustainable and efficient aviation sector.

Keywords
Additional aerodynamic surfaces (wingtips, winglet), Airplane appearance, Choice of parameters, Element design, Vector of parameters.

References
[1] G. Corrado et al., “Recent Progress, Challengesand Outlook for Multidisciplinary Structural Optimization of Aircraft and Aerial Vehicles,” Progress in Aerospace Sciences, vol. 135, pp. 100861, 2022.
[CrossRef] [Google Scholar] [Publisher Link]
[2] Yuping Wang et al., “Aerodynamic Performance of the Flexibility of Corrugated Dragonfly Wings in Flapping Flight,”Acta Mechanica Sinica/Lixue Xuebaom, vol. 38, no. 11, 2022.
[CrossRef] [Google Scholar] [Publisher Link]
[3] J.E. Guerrero, M. Sanguineti, and K. Wittkowski, “Variable Cant Angle Winglets for Improvement of Aircraft Flight Performance,” Meccanica, vol. 55, no. 10, pp. 1917-1947, 2020.
[CrossRef] [Google Scholar] [Publisher Link]
[4] Wengang Chen et al., “Shape Optimization to Improve the Transonic Fluid-Structure Interaction Stability by an Aerodynamic Unsteady Adjoint Method,” Aerospace Science and Technology, vol. 103, 2020.
[CrossRef] [Google Scholar] [Publisher Link]
[5] Gang Wang et al., “Deployment Modes and Aerodynamic Analysis of UAV Orthogonal Biaxial Folding Wing,” Aerospace, vol. 10, no. 1, p. 26, 2023.
[CrossRef] [Google Scholar] [Publisher Link]
[6] Hiroki Mukohara, and Masayuki Anyoji, “Computational Analysis of Compressibility Effect on Flow Fieldand Aerodynamics at Low Reynolds Numbers,” Physics of Fluids, vol. 34, no. 51, 2022.
[CrossRef] [Google Scholar] [Publisher Link]
[7] Shiva Prasad Uppu et al., “High-Speed Flow Over Airfoils, Wings and Airplane Configurations,” Handbook of Research on Aspects and Applications of Incompressible and Compressible Aerodynamics, pp. 230-254, 2022.
[CrossRef] [Google Scholar] [Publisher Link]
[8] Chukwugozie Ejeh et al., “Investigating the Impact of Velocity Fluctuationsand Compressibility to Aerodynamic Efficiency of a Fixed-Wing Aircraft,” Results in Physics, vol. 18, 2020.
[CrossRef] [Google Scholar] [Publisher Link]
[9] Shuichi Hiramatsu et al., “Aeroelastic Deformation Measurement of Martian Airplane for High-Altitude Flight Experiment Using Stereophotogrammetry,” Engineering Research Express, vol. 3, no. 1, 2021.
[CrossRef] [Google Scholar] [Publisher Link]
[10] Like Xie et al., “Improving Aircraft Aerodynamic Performance with Bionic Wing Obtained by Ice Shape Modulation,” Chinese Journal of Aeronautics, vol. 36, no. 2, pp. 76 – 86, 2023.
[CrossRef] [Google Scholar] [Publisher Link]
[11] Ignazio Dimino, “Integrated Design of a Morphing Winglet for Active Load Controland Alleviation of Turboprop Regional Aircraft,” Applied Sciences, vo1.1, no. 5, pp. 127, 2021.
[CrossRef] [Google Scholar] [Publisher Link]
[12] I. B. Manjunath, V. M. Kulkarni, and P. Balaraman, “Geometry Optimization Studies on Nonplanar Wingtip Devices for Typical Transport Aircraft,” Journal of Physics: Conference Series. vol. 1473, no. 1, 2020.
[CrossRef] [Google Scholar] [Publisher Link]
[13] C. Conlan-Smith et al., “Aerodynamic Shape Optimization of Aircraft Wings Using Panel Methods, “American Institute of Aeronautics and Astronautics Journal, vol. 58, no. 9, pp. 3765-3776, 2020.
[CrossRef] [Google Scholar] [Publisher Link]
[14] Hadar Ben-Gida, and R. Gurka, “The Leading-Edge Vortex Over a Swift-Like High-Aspect-Ratio Wing with Nonlinear Swept-Back Geometry,” Bioinspiration and Biomimetics. vol. 17, no. 6, 2022.
[CrossRef] [Google Scholar] [Publisher Link]
[15] M. A. Poghosyan, Ed., Proektirovanie Samoletov, Aircraft Design, Moscow, Russia: Innovacionnoe Mashinostroenie, 2018.
[16] D. P. Raymer, Aircraft Design: A Conceptual Approach, Aerspace Research Central, 1992.
[17] Pratheepan.J, and Bruce Ralphin Rose. J, "Aileron Effectiveness in the Presence of Aeroelastic Deformations," SSRG International Journal of Mechanical Engineering, vol. 2, no. 6, pp. 12-16, 2015.
[CrossRef] [Google Scholar] [Publisher Link]
[18] Nishant Kumar, Saurav Upadhaya, and Ashish Rohilla, "Evaluation of the Turbulence Models for the Simulation of the Flow Over a Tsentralniy Aerogidrodinamicheskey Institut (TsAGI)-12% Airfoil," SSRG International Journal of Mechanical Engineering, vol. 4, no. 1, pp. 18-28, 2017.
[CrossRef] [Google Scholar] [Publisher Link]
[19] I. A. Belov et al., Problems and Methods for Calculating Separated Flows of an Incompressible Fluid, Leningrad, USSR: Sudostroenie, 1989.
[20] V. T. Kalugin et al., Aerodinamicheskie Truby Dozvukovykh I Sverkhzvukovykh Skorostej, Aerodynamic Tubes of Subsonic and Supersonic Velocities, Moscow, Russia: Publishing House of Bauman Moscow State Technical University, 2004.
[21] S. Khan, and S. Sharma, “Analysis of Cloud Computing for Security Issuesand Approaches,” International Journal on Emerging Technologies, vol. 10, no. 1, pp. 68-73, 2019.
[Google Scholar] [Publisher Link]
[22] Victor Maldonado et al, “Active Flow Control as a Technique To Improve Fixed-Wingand Rotary-Wing Aerodynamics of Uavs,” AUVSI XPONENTIAL 2020, 2020.
[Google Scholar] [Publisher Link]
[23] Md Rafiqur Rahman, "Computational Analysis of Aerodynamic Parameters for Supersonic Artillery Projectiles," SSRG International Journal of Mechanical Engineering, vol. 7, no. 8, pp. 5-17, 2020.
[CrossRef] [Google Scholar] [Publisher Link]
[24] M. Zhao et al., “Dynamic Stall of Pitching Tubercled Wings in Vortical Wake Flowfield,” Physics of Fluids, vol. 35, no. 1, 2023.
[CrossRef] [Google Scholar] [Publisher Link]
[25] A. G. Bratuhin, Ed., Mezhdunarodnaya Enciklopediya CALS. Aviacionno-Kosmicheskoe Mashinostroenie [International Encyclopedia CALS. Aerospace Engineering]. Moscow, Russia: NIC ASK, 2015.
[26] K. P. Petrov, Aerodinamika Elementov Letatelnykh Apparatov [Aerodynamics of Aircraft Elements]. Moscow, USSR: Mashinostroenie, 1985.
[Google Scholar]
[27] Hyoungjin Kim, and May-Fun Liou, “Flow Simulationand Drag Decomposition Study of N3-X Hybrid Wing-Body Configuration,” Aerospace Science and Technology, vol. 85, pp. 24 – 39, 2019.
[CrossRef] [Google Scholar] [Publisher Link]