User:Utsav Chakraborty/sandbox

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Utsav Chakraborty
Aerospace Engineer
Born26/02/2005
Arambagh
OccupationStudent
ParentMr. Prasanna Chakraborty & Mrs. Indira Chakraborty

Utsav Chakraborty (26/02/2005) can be a lead-in to the Aerospace Engineering. Indian and Research scholar and student of Aerospace Engineering. Having three research paper in the field of Propulsion and Aerodynamics.

Biography

He has completed his AISSE from KV BSF Krishnanagar in 2020 with 87.6%. He has completed his AISSCE from KV Tarakeswar in 2022 with 80.2%. And right now, he is a student at Chandigarh University, studying BE in Aerospace Engineering. He has also completed UAV design part 2 from Swayam NPTEL in collaboration with IIT Kanpur and awarded with Elite Certificate. He has passed Machine Learning from IIT Bhubaneshwar in collaboration with Teachnook. He has passed Introduction to Microsoft Excel from Coursera. He has three research paper 1."Effects of Simulated Surface Roughness on Flow Characteristics in Symmetrical Airfoil"

2."Influence of Surface Roughness on Symmetric Airfoil Flow Properties and Reynolds Number" accredited by IJSREM(INTERNATIONAL JOURNAL OF SCIENTIFIC RESEARCH IN ENGINEERING AND MANAGEMENT) with impact factor of 8.4 and 3." Investigating Flame Stabilization using Chakraborty / U- Shape Flame Holder" accredited by JNRID(JOURNAL OF NOVEL RESEARCH AND INNOVATIVE DEVELOPMENT) with impact factor of 9.57

Early life

Born in a middle-class family in 2005, Chakraborty was studied in CBSE accredited Central Govt. School i.e., Kendriya Vidyalaya BSF Krishnanagar for completing his AISSE and then move to Kendriya Vidyalaya Tarakeswar for completing his AISSCE. Since childhood, Chakraborty and his parents wants that he should choose some branch which is something interesting and different. So, he is admitted in Chandigarh University for studying BE in Aerospace Engineering after qualifying CUCET.

Published works

1."Effects of Simulated Surface Roughness on Flow Characteristics in Symmetrical Airfoil" is published in the journal "International Journal of Scientific Research in Engineering and Management" (IJSREM) on Volume 08, Issue 04 April 2024. Here in this research, Chakraborty and two of his co researchers made one symmetric airfoil where they introduced slight roughness with the help of the sandpaper and found that Drag reduction capacity according to the above two documents: If well designed and used, control roughness should be reduced - according to research studies and wing roughness theory, drag examined to reduce in the range of is 2.799813345776948%. 2."Influence of Surface Roughness on Symmetric Airfoil Flow Properties and Reynolds Number" is published in the journal "International Journal of Scientific Research in Engineering and Management" (IJSREM) on Volume 08, Issue 05 May 2024.

Here in this research, Chakraborty and two of his co researchers made one symmetric airfoil where they introduced slight roughness with the help of the sandpaper and found that with proper design and application, the control roughness should be reduced. According to research studies and blade roughness theory, the Reynolds number has been studied in the range of 1.699495868%.

3." Investigating Flame Stabilization using Chakraborty / U- Shape Flame Holder" is published in the journal "JOURNAL OF NOVEL RESEARCH AND INNOVATIVE DEVELOPMENT" (JNRID) on Volume 02, Issue 05 May 2024.

Here in this research, Chakraborty and two of his co researchers made U shaped flame holder where they found that with proper design and application, the importance of the recirculation zones in anchoring the flame can be verified by visualizing them behind the 

Chakraborty / U-shaped structure. According to Flame stabilization studies in a bluff-body burner using combined numerical and experimental approaches Experimental and Computational Investigation of Flame Holders in Combustion Chambers at Different Thermal Loads and found that the model is properly designed, then the efficiency will be maximum of 98.9 %.

Recognition

Recognized as scholar by ABCD High Index. Recognized as Research Reviewer by JOURNAL OF NOVEL RESEARCH AND INNOVATIVE DEVELOPMENT" (JNRID) & International Journal of Innovative Research and Technology.

See also

www.linkedin.com/in/utsav-chakraborty-7129a124a

References/Notes and references

https://abcdindex.com/reviewer/utsav-chakraborty-000-518-252 https://www.researchgate.net/profile/Utsav-Chakraborty-2 https://chandigarhuniversity.academia.edu/UtsavChakraborty

Further reading

https://www.researchgate.net/publication/380728342_Effects_of_Simulated_Surface_Roughness_on_Flow_Characteristics_in_Symmetrical_Airfoil

https://www.researchgate.net/publication/380728350_Influence_of_Surface_Roughness_on_Symmetric_Airfoil_Flow_Properties_and_Reynolds_Number

https://www.researchgate.net/publication/380734717_Investigating_Flame_Stabilization_using_Chakraborty_U-Shape_Flame_Holder?_tp=eyJjb250ZXh0Ijp7ImZpcnN0UGFnZSI6InByb2ZpbGUiLCJwYWdlIjoicHJvZmlsZSIsInByZXZpb3VzUGFnZSI6InB1YmxpY2F0aW9uIn19