A Review on Airfoils with Serrated Trailing edge

Authors

  • Neel N. Zalavadia P.G. Student Mechanical Engineering Department, BVM Engineering College, V.V. Nagar, Anand, Gujarat, India
  • M.J. Zinzuvadia Associate Professor Mechanical Engineering Department, BVM Engineering College, V.V. Nagar, Anand, Gujarat, India
  • V.H. Chaudhari Assistant Professor Mechanical Engineering Department, BVM Engineering College, V.V. Nagar, Anand, Gujarat, India

Keywords:

Airfoils, Serration, Leading Edge, Trailing edge, Acoustic Emission

Abstract

 This Review paper gives a brief introduction the effects of providing the serration in airfoils. Few experimental procedures have been presented in this review paper in order to understand the effect of introducing serration. Major factor affecting by serration is the noise emission due to turbulence and boundary layer separation. The Acoustic levels are found to be decreasing by the use of serration and the aerodynamic properties like lift force drag force remains same. Presently all conclusion are based on the experimental work and empirical derivation

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Published

2018-05-28

How to Cite

Zalavadia, N. N. ., Zinzuvadia, . M., & Chaudhari, V. . (2018). A Review on Airfoils with Serrated Trailing edge. International Journal of Technical Innovation in Modern Engineering & Science, 4(5), 178–185. Retrieved from https://ijtimes.com/index.php/ijtimes/article/view/1437

Issue

Vol. 4 No. 5 (2018): Vol. 4 No. 5: Volume 4 Issue 5 (May-2018)

Section

Articles