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1(3), (2022):22-28. DOI: https://doi.org/10.46632/jdaai/1/3/4
Rohi Bindal, Ankit Kumar Mishra
The principles of flight deals with the motion of air and forces acting on an aircraft. The theoretical aspects of aircraft deals with four different forces. The main aim of the study was to analyse the Swept Back Wing for Supersonic and Hypersonic Mach Regimes at various angles of attack. The geometry and analysis were done using Ansys-Fluent. Calculations were done for constant air velocity altering only the angle of attack. The findings present up the contours of pressure and velocity along with evaluation of lift, drag and its coefficients.
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AdvaitInamdar, Narayan Thakur, Deepak Pal, Akshat Mohite, FLEXIBLE WING STRUCTURE AND VARIABLE-SWEEP WING MECHANISM, International Research Journal of Engineering and Technology (IRJET), 8(3), 2021
Radhakrishnan P, Ramanan G, Chandan Gowda H R,Meghana C K, Chaithra A N, Aerodynamic Performance Analysis of a Variable Sweep Wing for Commercial Aircraft Applications, ACS Journal for Science and Engineering, 1(1), 2021, https://doi.org/10.34293/acsjse.v1i1.5
Gao, G.X.Xiang, W. J.Tang, X. Z. Jie, X. Huang, J.Y. He, S.A. Liu, Investigations on the complex fows induced by dual-swept/dual ramp wedges in supersonic fows, Sci Rep, 10 2020, https://doi.org/10.1038/s41598-020-66676-5
Hao Zhou, Gang Wang, Zhikan Liu, Numerical analysis on flutter of Busemann-type supersonic biplane air foil, Journal of Fluids and Structures, 92, 2020, https://doi.org/10.1016/j.jfluidstructs.2019.102788
Nao Setoguchi, Masahiro Kanazaki, Low-Speed and High Angle of Attack Aerodynamic Characteristics of Supersonic Business Jet with Forward Swept Wing, AIAA Scitech 2020 Forum, 2020, DOI: 10.2514/6.2020-0534
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Yuki Kishi, Shinya Kitazaki, AtthaphonAriyarit, Yoshikazu Makino, Masahiro Kanazaki, Planform dependency of optimum cross-sectional geometric distributions for supersonic wing,90, 2019, pp. 181-193, https://doi.org/10.1016/j.ast.2019.03.057
Cheng Gong, Bao-Feng Ma, Shape Optimization and Sensitivity Analysis of a Morphing-Wing Aircraft, International Journal of Aeronautical and Space Sciences, 20,2019, pp. 57-69, https://doi.org/10.1007/s42405-018-0110-7
Jenna L. Eppink, Richard W. Wlezien, Rudolph A. King, MeelanChoudhari, Influence of a Backward-Facing Step on Swept-Wing Boundary-Layer Transition, AIAA JOURNAL, 57(1), 2018, https://doi.org/10.2514/1.J057437
Saya Mochizuki, Gouji Yamada, Aerodynamic characteristics and flow field of delta wings with the canard, MATEC Web of Conferences, 145, 2018, https://doi.org/10.1051/matecconf/201814503010
Dinesh Aravinth, ParitoshShinde, Ajay Misra, Mahesh M. Sucheendran, HamedFaghanpourGanji, DYNAMIC AEROELASTICITY OF A TRAPEZOIDAL WING USING ENHANCED PISTON THEORY,2018, DOI: 10.2514/6.2018-1443
Rohi Bindal, Ankit Kumar Mishra, “Theoretical and Computational Investigation on Swept Back Wing using CFD Method, “REST Journal on Advances in Mechanical Engineering, 1(3), (2022):22-28.