Browse > Article
http://dx.doi.org/10.20910/JASE.2022.16.1.81

A Study on the Structural Design and Analysis of Air Intake of Unmanned Aerial Vehicles Applied to Composite Materials  

Choi, Heeju (KIPCO)
Park, Hyunbum (School of Mechanical Convergence System Engineering, Kunsan National University)
Publication Information
Journal of Aerospace System Engineering / v.16, no.1, 2022 , pp. 81-85 More about this Journal
Abstract
In this study, we conducted a structural design and analysis of air intake of aircraft engine using composite materials. First, an investigation on structural design requirement of target structure was carried out. The distributed pressure load and acceleration condition was applied to structural design. To evaluate the structural design result, finite element analysis was carried out. The stress, deflection and buckling analysis for structural safety evaluation was performed. Finally, it was confirmed that the air intake through structural analysis is safety.
Keywords
Composite Material; Air Intake; Structural Design; Structural Analysis;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
1 Guoping Huang, Fengyuan Zuo, Wenyou Qiao, "Design method of internal waverider inlet under non-uniform upstream for inlet/forebody integration," Aerospace Science and Technology, Vol. 74, pp. 160-172, 2018.   DOI
2 Pedro David Bravo-Mosquera, Alvaro Martins Abdalla, Hernan Dario Ceron-Munoz, Fernando Martini Catalano., "Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraft," Aerospace Science and Technology, Vol. 86, pp. 497-519, 2019.   DOI
3 Vittorio Vercillo, Norbert Karpen , Alexandre Laroche, Javier A. M. Guillen, Simone Tonnicchia, Raphael de Andrade Jorge, Elmar Bonaccurso, "Analysis and modelling of icing of air intake protection grids of aircraft engines," Cold Regions Science and Technology, Vol. 160, pp. 265-272, 2019.   DOI
4 F. Bagnoli, M. Bernabei, A. Ciliberto, "Failure analysis of an aircraft auxiliary power unit air intake door," Engineering Failure Analysis, Vol. 18, pp. 284-294, 2011.   DOI
5 Mohammad R Soltani, Javad Sepahi Younsi, Mohammad Farahani, Afshin Masoud, "Numerical simulation and parametric study of a supersonic intake," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 227, pp. 106490, 2013.
6 Lee M. Berra, John W. Slater, Semih M. Olcmen, "Conceptual redesign of the B-1B bomber inlets for improved supersonic performance," Aerospace Science and Technology, Vol. 45, pp. 476-483, 2015.   DOI
7 Bae, H., Lee, S., Kim, Y., Jeong, I., Lee, S., Cho, D., "Probabilistic Approach for Fighter Inlet Hammershock Design Pressure," Journal of Aerospace System Engineering, Vol. 13, No. 5, pp. 72-78, 2019.   DOI
8 Lee, J., Lee, K., Kho, S., Kwak, J., "Inlet distortion test of gas turbine engine," Journal of Aerospace System Engineering, Vol. 1, No. 1, pp. 53-59, 2007.
9 Shuvayan Brahmachary, Chihiro Fujio, Hideaki Ogawa, "Multi-point design optimization of a high-performance intake for scramjet-powered ascent flight," Aerospace Science and Technology, Vol. 107, pp. 106362, 2020.   DOI
10 Zeyang Zhou, Jun Huang, "Mixed design of radar/infrared stealth for advanced fighter intake and exhaust system," Aerospace Science and Technology, Vol. 110, pp. 106490, 2021.   DOI
11 Kang, M., Park, D., Kang, H., Lee, S., "Performance Analysis based on Impller Inlet & Outlet Angle for Waterjet," Journal of Aerospace System Engineering, Vol. 5, No. 2, pp. 27-32, 2011.   DOI
12 H. Kim, M. S. Liou, "Shape design optimization of embedded engine inlets for N2B hybrid wing-body configuration," Aerospace Science and Technology, Vol. 30, pp. 128-149, 2013.   DOI
13 Wenbiao Gan, Xiaocui Zhang, "Design optimization of a three-dimensional diffusing S-duct using a modified SST turbulent model," Aerospace Science and Technology, Vol. 63, pp. 63-72, 2017.   DOI