This paper is published in Volume-2, Issue-4, 2016
Area
CFD
Author
Ashish Kumar Saroj, Bharath Reddy, Gundu Jayadhar, D.Gokul
Org/Univ
XPLOCC Technologies, Lucknow, India
Keywords
Grooved cylinder, Angular velocity, Reynolds number, laminar, Incompressible fluid, Wake region.
Citations
IEEE
Ashish Kumar Saroj, Bharath Reddy, Gundu Jayadhar, D.Gokul. Flow Past a Rotating Circular Grooved Cylinder, International Journal of Advance Research, Ideas and Innovations in Technology, www.IJARIIT.com.
APA
Ashish Kumar Saroj, Bharath Reddy, Gundu Jayadhar, D.Gokul (2016). Flow Past a Rotating Circular Grooved Cylinder. International Journal of Advance Research, Ideas and Innovations in Technology, 2(4) www.IJARIIT.com.
MLA
Ashish Kumar Saroj, Bharath Reddy, Gundu Jayadhar, D.Gokul. "Flow Past a Rotating Circular Grooved Cylinder." International Journal of Advance Research, Ideas and Innovations in Technology 2.4 (2016). www.IJARIIT.com.
Ashish Kumar Saroj, Bharath Reddy, Gundu Jayadhar, D.Gokul. Flow Past a Rotating Circular Grooved Cylinder, International Journal of Advance Research, Ideas and Innovations in Technology, www.IJARIIT.com.
APA
Ashish Kumar Saroj, Bharath Reddy, Gundu Jayadhar, D.Gokul (2016). Flow Past a Rotating Circular Grooved Cylinder. International Journal of Advance Research, Ideas and Innovations in Technology, 2(4) www.IJARIIT.com.
MLA
Ashish Kumar Saroj, Bharath Reddy, Gundu Jayadhar, D.Gokul. "Flow Past a Rotating Circular Grooved Cylinder." International Journal of Advance Research, Ideas and Innovations in Technology 2.4 (2016). www.IJARIIT.com.
Abstract
CFD simulations of a two-dimensional steady state flow past a rotating circular grooved cylinder is analyzed in this study. Cylinder of diameter 0.1 m with 8 grooves of 0.01 m was examined at various Reynolds’s number (0.1 to 50) and angular velocity (0 to 100 RPS). Incompressible Navier Stokes equation in Ansys Fluent 14.0 was used to examine the flow. The pressure and velocity contours for various Reynolds’s number were generated. The result suggested that the flow remains attached to the surface of the cylinder up to the Reynolds number value of 4–5 and the flow pattern was independent of angular velocity at Reynolds’s number 45-46 and the cylinder behaved like a stationary cylinder and above these Reynolds’s numbers the flow is still two-dimensional, but no longer steady.