Study of flow by varying the position of maximum chamber thickness on aerofoil
Department of Mechanical Engineering, Pragati Engineering College, Surampalem, Kakinada 533001, India
Ganesh Nathipam
Department of Mechanical Engineering, Pragati Engineering College, Surampalem, Kakinada 533001, India
Sri Ram Deepak Akella
Department of Mechanical Engineering, Pragati Engineering College, Surampalem, Kakinada 533001, India
Phani Bhaskar Anusuri
Department of Mechanical Engineering, Pragati Engineering College, Surampalem, Kakinada 533001, India
DOI: https://doi.org/10.52542/tjdu.1.2.69-75
Keywords: chamber thickness, angle of attack, CFD, lineation’s, linear regression
Abstract
Aerofoil is a design with a curved exterior that gives the most commendable ratio of lift to drag. The aerofoil which allows for the flow at a margin range of angle has a more remarkable impact on the power spawning from the turbine. The conception and examination for the airfoil Structure have been implemented in the current work to raise the behavior of the flow with a commendatory condition by varying the position of maximum chamber thickness position thereby varying the angle of attack with 5 degrees interval from 0-25 degrees. The best model is studied with surface modifications to increase the flow separation and efficiency of lift.
References
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Published
2021-08-27
How to Cite
Jithendra Sai Raja Chada, Ganesh Nathipam, Sri Ram Deepak Akella, Phani Bhaskar Anusuri, “Study of flow by varying the position of maximum chamber thickness on aerofoil”, Technical Journal of Daukeyev University, Vol. 1, Issue 2, 2021, pp. 69-75.
Issue
Volume 1, Issue 2 (2021)
Section
Article
Copyright © 2021 Jithendra Sai Raja Chada, Ganesh Nathipam, Sri Ram Deepak Akella, Phani Bhaskar Anusuri
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Copyright © 2021 Jithendra Sai Raja Chada, Ganesh Nathipam, Sri Ram Deepak Akella, Phani Bhaskar Anusuri
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