Ministry of Education
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Prof Dhwanil Shukla

vidwan id: 155732
Male

Professor, Department of Aerospace Engineering
Indian Institute of Technology Bombay

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Expertise

  • Aerospace Engineering

Publications

Total Articles 40
Books 0
Proceedings 0

Publications

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Scopus

Citations 406
h-index 8

CrossRef

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Citations 57
h-index 4
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Professional Recognition

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Bio

Aerodynamics

Personal Details

  • Male
  • Professor , Indian Institute of Technology Bombay
  • Indian Institute of Technology Bombay, Powai
Ph.D
Other Institute 2019
Professor Apr 2018 – Present
Indian Institute of Technology Bombay | Department of Aerospace Engineering

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Co-Authors (1)

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Scholarly Work

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Scholarly Publications

Performance of Isolated UAV Rotors at Low Reynolds Number

Open Access
Conference Paper
Year: 2020. Volume: 2020-March , Issue: March .
Authors: Tomar Y.;Shukla D.;Komerath N.
DOI 10.4271/2020-01-0046

Interactions of two UAV rotors at low reynolds number

Open Access
Conference Paper
Year: 2020. Volume: 1 .
Authors: Tomar Y.;Shukla D.;Komerath N.
DOI 10.1115/FEDSM2020-20108
1

An experimental investigation of rotor-box aerodynamic interaction

Open Access
Article
Year: 2019. Volume: 141 , Issue: 12 .
Authors: Shukla D.;Komerath N.
DOI 10.1115/1.4043951
1 2

Rotor wake and inflow characteristics of multirotor drone configurations

Open Access
Conference Paper
Year: 2019. Volume: 2 , Pages: 1511-1519 .
Authors: Chen P.W.;Shukla D.;Sankar L.;Komerath N.;Prasad J.V.R.
2

Drone scale coaxial rotor aerodynamic interactions investigation

Open Access
Article
Year: 2019. Volume: 141 , Issue: 7 .
Authors: Shukla D.;Komerath N.
DOI 10.1115/1.4042162
6 36

Rotor–duct aerodynamic and acoustic interactions at low Reynolds number

Open Access
Article
Experiments in Fluids. Year: 2019. Volume: 60 , Issue: 1 .
Authors: Shukla D.;Komerath N.
DOI 10.1007/s00348-018-2668-z
4 19

Low Reynolds number multirotor aerodynamic wake interactions

Open Access
Article
Experiments in Fluids. Year: 2019. Volume: 60 , Issue: 4 .
Authors: Shukla D.;Komerath N.
DOI 10.1007/s00348-019-2724-3
2 36

Vortical lift on retreating rotor blades at high advance ratios: The aerodynamics of the sharp edge vortex

Open Access
Article
Experiments in Fluids. Year: 2019. Volume: 60 , Issue: 6 .
Authors: Hiremath N.;Shukla D.;Komerath N.
DOI 10.1007/s00348-019-2740-3
6