Interference Effect between Prismatic Buildings Subjected to Microburst Wind

Authors

  • Kalyan Kumar Das Associate Professor ,Department of Industrial and Production Engineering,Assam Engineering College, Jalukbari,Guwahati,Assam-781013 ,India Email Id: kkdas1971[at]gmail[dot]com
  • Kalyan Prasad Sinhamahapatra
  • Amit Kumar Ghosh

DOI:

https://doi.org/10.3759/joise.v1i1.3487

Abstract

Severe thunderstorms are important weather phenomena which impact on various facets of national activity like civil and defense operation, particularly aviation, space vehicle launching and agriculture in addition to its damage potential to life and properties. One of the most important events in the thunderstorms is the “Downburst”. Downbursts occur when a column of descending air reaches the ground and bursts out violently. This downward motion abruptly changes direction and produces a peak wind speed close to the ground. A synoptic, or atmospheric boundary layer (ABL) wind however does not reach its maximum wind speed until much higher above the earth's surface.  It is believed that downburst is generated when the moist buoyant air moving upward can no longer be sustained above and subsides into downdraft. Downbursts can be wet (accompanying rain) or dry and are further classified as either microburst or macroburst depending on their horizontal extent of damage. In India severe thunderstorms over the Gangetic West Bengal and Assam, known as “Kalbaishakhi” and “Bordoisila” respectively are very much destructive. In this work an attempt has been made to simulate the dry downburst wind numerically using the impinging jet model of the downburst.  A CFD code is developed for the numerical simulation based on the vorticity-vector potential approach using a Large Eddy Simulation (LES) technique for the turbulence. The primary objectives of the present work are to investigate the flow dynamics of the downburst wind and its effect on prismatic buildings. The numerical results generated for the downburst wind profile are compared with the experimental results obtained from the physical microburst simulator developed by the authors with a 500 mm diameter jet and also with the available full scale data. Very good agreement is observed.

References

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Published

2019-11-18

Issue

Vol. 1 No. 1 (2014)

Section

Articles

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