Results 1 to 10 of about 48,655 (212)
Numerical simulation of the transition flight aerodynamics of cross-shaped quad-tiltrotor UAV [PDF]
Scientific ReportsIn order to enhance the stability of the tilt transition process, a new configuration of Quad-Tiltrotor UAV was presented in this paper. Firstly, numerical simulation was used to calculate and analyze the aerodynamic interaction between the front rotor ...
Siliang Du, Yi Zha
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FUSELAGE SHAPE OPTIMIZATION AIMED AT WING-FUSELAGE CONFIGURATION DRAG REDUCTION AT SUPERSONIC SPEEDS
Научный вестник МГТУ ГА, 2017 The problem of fuselage shape optimization of the wing-body configuration is considered in the following three formulations. In the first one, the angle of attack is fixed and equal to zero, the wing has a symmetric airfoil, and the fuselage is based on ...
N. D. Ageev, A. A. Pavlenko
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Empennage sizing with the tail volume complemented with a method for dorsal fin layout [PDF]
INCAS Bulletin, 2021 Purpose: Provide good values for the tail volume coefficient and the lever arm as a percentage of the fuselage length. Provide a statistical method for dorsal fin layout.
Dieter SCHOLZ
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Aerospace, 2023 This present study investigated the potential of passive flow control to reduce induced drag by using a micro-vortex generator (MVG) at a backward-facing step (BFS) location.
Zinnyrah Methal +5 more
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Contribution ofWing, Vertical Tail and Fuselage on Airplane Stability with Failed Outboard Engine [PDF]
Engineering and Technology Journal, 2009 The Effect of wing, vertical tail, and fuselage design parameters on airplane stabilitywith failed outboard engine presents in this study. Boeing (747-400) have been selectedfor available data.
Mohamed A. R.Yass +2 more
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Rekayasa Mesin, 2022 To improve the application and use value of Palm Oil Empty Fruit Bunch (OPEFB) waste as a composite material, the research team conducted research related to the utilization OPEFB fiber as an alternative material to replace carbon fiber in the ...
Kaspul Anuar +2 more
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Research on Calculation Method for Acoustic Scattering of Helicopter Noise
Xibei Gongye Daxue Xuebao, 2020 A new calculation method of helicopter rotor/fuselage acoustic scattering is developed. Firstly, a CFD analysis model is developed to simulate flow field of the rotor, which is based on the motional embedded grid system and RANS equations, and provides ...
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Acta Acustica, 2022 The main acoustic noise source of helicopters is supposed to be the rotor blades, but the scattering effect of the helicopter fuselage sometimes cannot be ignored.
Wang Zeyang, Huang Jun, Yi Mingxu
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European Mechanical Science, 2023 In this study, numerical analysis of the fuselage of a rotary wing unmanned aerial vehicle was conducted. A fuselage that is resistant to the loads on the fuselage and has maximum lightness has been designed.
Metin Uzun +3 more
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Waste analysis of fuselage assembly in panelization group of the 117th NC212i aircraft
Jurnal Sistem dan Manajemen Industri, 2020 Dirgantara Indonesia (PTDI) is the single source producer of the NC212i Aircraft. Almost every Aircraft is delivered to the customer over the deadline date. The existence of waste is believed to be one of causing the late delivery.
Frisca Pomalia +2 more
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