TY - GEN
T1 - Unsteady flow characteristics and viscous flow losses behind multiple rows of circular pin fins in coolant channels
AU - Gokce, Zeki Ozgur
AU - Camci, Cengiz
PY - 2011
Y1 - 2011
N2 - This article deals with a computational assessment of 3D viscous flow behind multiple rows of circular pin fins in coolant channels used in gas turbine systems. Unsteady oscillations and turbulent flow characteristics especially near the endwall surfaces generate the much needed heat transfer enhancement that is usually from the walls to the coolant fluid. The current study is about a comprehensive assessment of present day computational fluid dynamics solvers for the enhancement of wall to coolant heat transfer rates. The paper presents details regarding many flow characteristics, including particle streamlines, as well as total pressure, turbulent kinetic energy and hub heat transfer coefficient contours. The endwall fence placed upstream of the cylinder generates a measurable increase in heat transfer rates downstream of the cylinder. The paper also includes a number of suggested ways to enhance endwall heat transfer rates for use in gas turbine cooling configurations and total pressure improvements near the turbine hub endwall.
AB - This article deals with a computational assessment of 3D viscous flow behind multiple rows of circular pin fins in coolant channels used in gas turbine systems. Unsteady oscillations and turbulent flow characteristics especially near the endwall surfaces generate the much needed heat transfer enhancement that is usually from the walls to the coolant fluid. The current study is about a comprehensive assessment of present day computational fluid dynamics solvers for the enhancement of wall to coolant heat transfer rates. The paper presents details regarding many flow characteristics, including particle streamlines, as well as total pressure, turbulent kinetic energy and hub heat transfer coefficient contours. The endwall fence placed upstream of the cylinder generates a measurable increase in heat transfer rates downstream of the cylinder. The paper also includes a number of suggested ways to enhance endwall heat transfer rates for use in gas turbine cooling configurations and total pressure improvements near the turbine hub endwall.
UR - http://www.scopus.com/inward/record.url?scp=84869160783&partnerID=8YFLogxK
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U2 - 10.1115/imece2011-64333
DO - 10.1115/imece2011-64333
M3 - Conference contribution
AN - SCOPUS:84869160783
SN - 9780791854877
T3 - ASME 2011 International Mechanical Engineering Congress and Exposition, IMECE 2011
SP - 11
EP - 21
BT - Advances in Aerospace Technology; Energy Water Nexus; Globalization of Engineering; Posters
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME 2011 International Mechanical Engineering Congress and Exposition, IMECE 2011
Y2 - 11 November 2011 through 17 November 2011
ER -