Fluid flow and heat transfer enhancement in wings with combined solid ring twisted tape inserts circular heat exchanger tube
| Autor: | Rajesh Maithani, Alok Darshan Kothiyal, Anil Kumar, Ravi Datt, Mangal Singh Bhist |
|---|---|
| Jazyk: | angličtina |
| Rok vydání: | 2019 |
| Předmět: |
Insert (composites)
Materials science twists ratio Renewable Energy Sustainability and the Environment 020209 energy Heat transfer enhancement multiple twisted tapes lcsh:Mechanical engineering and machinery Reynolds number wing pitch ratio 02 engineering and technology wing depth ratio and solid rings symbols.namesake Heat transfer Thermal Heat exchanger 0202 electrical engineering electronic engineering information engineering symbols Fluid dynamics lcsh:TJ1-1570 Tube (container) Composite material heat transfer enhancement |
| Zdroj: | Thermal Science, Vol 23, Iss 6 Part B, Pp 3893-3903 (2019) |
| ISSN: | 0354-9836 |
| Popis: | Experimental examination is carried out to study the turbulent heat transfer and fluid-flow characteristics in circular heat exchanger tube using combined wing with solid ring twisted tape inserts. A series of experiments has been performed with the range of Reynolds number varied from 3000 to 21000, number of twisted taped inserts, NTT, varied from 1.0 to 4.0 with constant value of other twisted tape parameters such as rings pitch ratio, dR /DT = 1.0, wing pitch ratio, PW /WT = = 3.0, and wing depth ratio, Wd /WT = 1.67. Based on the examined, turbulent heat transfer and fluid-flow in wing with combined solid ring twisted tape inserts results are compared with plain circular tube under same operating conditions. The experimental results show that the heat transfer is increased around 5.66 times than plane circular heat exchanger tube. The thermal and hydrodynamic performance parameter based on equal pumping power, ?p, was found to be highest for NTT = 3.0. The optimum value of thermal and hydrodynamic performance has been found to be 2.74 for Reynolds mumber of 3000 within the range of the parameters investigated. Multiple wings with solid rings twisted tape inserts have been also shown to be thermally as well as hydraulically better in comparison to other similar twisted tape insert geometries. |
| Databáze: | OpenAIRE |
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