Wireless sensor networks are applied in different fields of human endeavor such as security services in military and police operations, civilian and commercial purposes. Their use is of increasing demand in the global society recently as the need for data gathering to solve big data problem is on the rise. Today, Internet of Things (IoT) is the technology being used to provide seamless remote operations in all fields using sensors that are wirelessly networked. Hence, considering the amount of that passing through these networks and the security required of them to ensure that privacy of data is concealed and secured; the need for providing adequate protection for WSNs while ensuring prolong operation by increasing their life span by ensuring energy saving capacity becomes very paramount. This paper has carried out empirical review of implemented techniques for energy preservation and privacy provision in WSNs.
- Page(s): 01-06
- Date of Publication: 21 December 2021
- Nwokonkwo, O.C. Department of Information Technology, Federal University of Technology, Owerri, Imo State- Nigeria
- Ofeogbu, C.I. Department of Computer Science, Federal University of Technology, Owerri, Imo State- Nigeria
- Njoku, O. A. Department of Computer Science, Federal University of Technology, Owerri, Imo State- Nigeria
- Madu, F.U. Department of Computer Science, Federal Polytechnic, Nekede, Owerri-Imo State
- Okeahialam, T.C. Department of Information Media Technology, Federal University of Technology, Minna, Niger State- Nigeria
- Ikwuazom, C. T. Department of Information Media Technology, Federal University of Technology, Minna, Niger State- Nigeria
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Nwokonkwo, O.C., Ofeogbu, C.I., Njoku, O. A., Madu, F.U., Okeahialam, T.C., Ikwuazom, C. T., "Review Techniques in Energy Conservation and Sink Node Privacy Preservation in Wireless Sensor Networks" International Journal of Latest Technology in Engineering, Management & Applied Science-IJLTEMAS vol.10 issue 11, November 2021, pp.01-06 URL: https://ijltemas.in/DigitalLibrary/Vol.10Issue11/01-06.pdf
Major structural part of an aircraft is the wing which is used to produce the lift during flying conditions. Wing is inclined at certain angle of attack with stall regions. When the flow passes over an airfoil due to the pressure difference at top and bottom surface of the wing the lift force is generated. The aim of the present study is to design the rectangular wing of subsonic aircraft using 3D EXPERIENCE &analysis through SIMULIA with Al alloy to find von-mises stress which is developed in the wing design.The wing is designed in solid modelling software using 3D EXPERIENCE and analysis is done using finite element method by using SIMULIA. Static structural analysis of the wing is done to find deformation, stress, and strain induced in the wing structure wing. Production of the lift to drag ratio for the tailless aircraft is high. The stability of an aircraft is considered for the flying wing is dependent on the design and configuration of the wing construction for production of lift in major conditions of flight. With the known values of von mises stress and displacements and strainsthe region of slip where the failure may occur and zones of failures are introduced before braking through rectanngular wing structural analysis.
- Neelima Pottabathini Department of Aerospace Engineering, Jain University, Jakkasandra Post, Kanakapura Road, Bangalore, India 562112
- Divya Mahesh Vaswani Department of Aerospace Engineering, Jain University, Jakkasandra Post, Kanakapura Road, Bangalore, India 562112
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Neelima Pottabathini & Divya Mahesh Vaswani, "Wing Design for Subsonic Aircraft" International Journal of Latest Technology in Engineering, Management & Applied Science-IJLTEMAS vol.10 issue 11, November 2021, pp.07-13 DOI: https://dx.doi.org/10.51583/IJLTEMAS.2021.101101