a0cb3b2f-75f0-4844-8368-9de23eca4b8b20240320075819876wseas:wseasmdt@crossref.orgMDT DepositDESIGN, CONSTRUCTION, MAINTENANCE2732-99842944-912X10.37394/232022https://wseas.com/journals/dcm/32020243202024410.37394/232022.2024.4https://wseas.com/journals/dcm/2024.phpMohamad Amiruddin BinIsmailDepartment of Technical and Vocational Universiti Pendidikan Sultan Idris 35900 Tanjung Malim, Perak MALAYSIAHendriPratamaDepartment of Technical and Vocational Universiti Pendidikan Sultan Idris 35900 Tanjung Malim, Perak MALAYSIAWan Nurlisa WanAhmadDepartment of Technical and Vocational Universiti Pendidikan Sultan Idris 35900 Tanjung Malim, Perak MALAYSIAIrdayanti Binti MatNashirDepartment of Technical and Vocational Universiti Pendidikan Sultan Idris 35900 Tanjung Malim, Perak MALAYSIALeeSoyoungKorean Armed Forced Nursing Academy 78-502, Yuseong-gu, Daejeon KOREAKazumaSekiguchiDepartment of Mechanical System Engineering Tokyo City University Tamazutsumi, Setagaya City, Tokyo 158-8557 JAPANThe design of the flying vehicles (FV) is becoming popular and it is very important nowadays. It is drafted in various circumstances and situations such as the military and transportation. The development of flying vehicles is different from ordinary airplanes because of its ability to fly in multiple directions. In this study, a new design for Malaysia was produced based on prototypes from previous models available in Japan. This design improved that it can has better stability of using fans and flaps on flying vehicles. This research paper is concerned with a flying vehicle that can fly a load of up to 480kg with a speed of up to 300km/h. This study is focusing on observed the existing flap design in the recognized literature for current flying vehicles. The plan accomplishes the energy efficiency of the flying vehicles. From the simulation of constraint diagram, the design of the aircraft was optimized; with the initial design of the wing, air foil designing with high performance of motor was done. Propeller and flap was design according to safety standard to fit in for the FV. The design of the new FV flap were compared to the existing model from the teTra aviation corp which was designed in Japan. The result of the new design FV flying vehicle will provide a clearer picture for the new concept that improvement flying time 35 % from the normal design.32020243202024161https://wseas.com/journals/dcm/2024/a02dcm-001(2024).pdf10.37394/232022.2024.4.1https://wseas.com/journals/dcm/2024/a02dcm-001(2024).pdf10.23919/sice48898.2020.9240434Wada, S., Sekiguchi, K., & Nonaka, K. (2020, September). Model predictive formation control for quadcopters with towing cables. In 2020 59th Annual Conference of the Society of Instrument and Control Engineers of Japan (SICE) (pp. 1275-1281). IEEE. https://doi.org/10.23919/SICE48898.2020.92 40434 Sei-Jin, Oh, “Flying Car”, The Korean Institute of Electrical Engineers, Vol. 16, No. 1, pp.27-30, 2019.1. 10.1016/j.ast.2020.106420Salgansky, E. A., & Lutsenko, N. A. (2021). Effect of solid fuel characteristics on operating conditions of low-temperature gas generator for high-speed flying vehicle. Aerospace Science and Technology, 109, 106420. https://doi.org/10.1016/j.ast.2020.106420 Ki Young Lee, H.G. Kim, C.H. Kim, G.J.Kang, Y.H. Kang, “Development of the Flying Car”, pp. 1184-1187(4 pages), The Korean Society for Aeronautical & Space Sciences, 2013.4. 2015]. http://dx.doi.org/10.15242/IIE.E0214015. Anderson, J. D. (1999). “Aircraft Performance and Design”, Elsevier publishers. Scribbr. https://cir.nii.ac.jp/crid/11302822722985123 84 Roskam, J. (1985). Airplane design VII: determination of stability, control and performance characteristics: Far and military requirements (Vol. 1). DARcorporation. Durand. W. F, Lesley. E. P, “Experimental research on air propellers”, NASA Technical reports Server, Available from: [16 September 2013]. Scribbr. https://ntrs.nasa.gov/citations/19930091041 Austin, R. (2011). Unmanned aircraft systems: UAVS design, development and deployment. John Wiley & Sons. Roy, B. (2000). Introduction to Aerospace Propulsion. Scribbr. http://103.62.146.201:8081/jspui/bitstream/1/ 8086/1/lec13-problem-solution.pdf. 10.2514/4.867538Nicolai Leland, M., & Carichner Grant, E. (2010). Fundamentals of Aircraft and Airship Design (AIAA Education Series). https://doi.org/10.1088/1757- 899X/376/1/012056 10.12928/joves.v2i1.761Nashir, I. M., Yusoff, A., Khairudin, M., Idris, M. R., & Ma’arof, N. I. (2019). Delphi Method: the Development of Robotic Learning Survey in Tertiary Education. Journal of Vocational Education Studies, 2(1), 13-22. Scribbr. https://core.ac.uk/download/pdf/267886324. pdf Fahlstrom, P. G., Gleason, T. J., & Sadraey, M. H. (2022). Introduction to UAV systems. John Wiley & Sons. 10.11113/jt.v78.9269Ismail, M. A., Muhamad, P., & Abu, A. (2016). Modelling and Design Smart Controller of Magneto Rheological Using Bouc-Wen and Sim Model for Motorcycle Suspension System. Jurnal Teknologi, 78(6-13), 31-36.