Author/Authors :
Arshad, H Department of Mechanical and Aeronautical Engineering - University of Engineering and Technology (UET), Taxila, Pakistan , Khushnood, S Department of Mechanical and Aeronautical Engineering - University of Engineering and Technology (UET), Taxila, Pakistan , Ahmad Nizam, L Department of Mechanical and Aeronautical Engineering - University of Engineering and Technology (UET), Taxila, Pakistan , Ameer Ahsan, M Department of Mechanical and Aeronautical Engineering - University of Engineering and Technology (UET), Taxila, Pakistan , Ghufran Bhatti, O Department of Mechanical and Aeronautical Engineering - University of Engineering and Technology (UET), Taxila, Pakistan
Abstract :
An experimental study is carried out on a parallel triangular finned tube array with P/Deff ratio 1.62 to
examine the effect of fin geometry on flow-induced vibration response. Fins on a tube increase the heat
transfer rate but these also affect the fluid dynamics around the tube. The flow pattern across the finned tubes
is complex as compared to bare tube arrays. There are numerous parameters that affect the finned tube
vibration subjected to air cross-flow in a tube array. In the current study, some of these parameters i.e. fin
thickness and fin density are focused and their effects on flow-induced vibration response are analyzed in
different rows of fin tube array. The current experimentation is performed in a subsonic wind tunnel using a
single flexible Aluminum finned tube in a rigid array. Seven tubes with similar specifications but distinct fin
thickness and fin density are used for the testing purpose. Their amplitude response suggests that the flowinduced
vibration behavior is greatly affected by changing the finned tube parameters. It has also been
observed during spectral analysis that the Strouhal number is independent of fin geometry since it remained
constant in different rows of the array for finned tubes under study. It suggests that the vortex shedding has
also contributed towards the finned tube vibration predominantly in the first, second and the fourth row of
tube array.
Keywords :
Parallel triangular , Fin geometry , Mass ratio , Flexible tube , Finned tube bundle