Vidwan-ID : 54441



  • Prof Gopalan Jagadeesh

  • Professor
  • Indian Institute of Science Bangalore
Publications 1996 - 2020

Publications

  • 89
    Journal Articles
  • 29
    Conference Paper
  • 2
    Note
  • 2
    Review
  • 1
    Chapter
  • 1
  • 21

Citations / H-Index

1025 Citations
19 h-index
218 Citations

Google Scholar

Co-author Network


Expertise

Experimental Hypersonics, Shock wave dynamics

Personal Information

Prof Gopalan Jagadeesh

Male
Aerospace Engineering Indian institute of science, Bangalore
India,Karnataka,Bangalore - 560012


Experience

  • Professor

    Indian Institute of Science Bangalore

  • Associate Professor

    Indian Institute of Science Bangalore

  • Assistant Professor

    Indian Institute of Science Bangalore


Qualification

  • Ph.D

    Indian Institute of Science, Bangalore

  • M.E

    Birla Institute of Technology MesraBirla Institute of Technology Mesra

  • B.E

    Bangalore University


Doctoral Theses Guided

2016

Experimental study of Shock – Shock Interactions in Hypersonic flows.

Abhishek Khatta, Indian Institute of Science

2015

Investigations on supersonic flows in miniature shock tubes.

Janardhanraj Subburaj, Indian Institute of Science

2015

Studies on impinging shock wave Boundary Layer Interactions.

Sriram R, Indian Institute of Science

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2016

Experimental study of Shock – Shock Interactions in Hypersonic flows.

Abhishek Khatta, Indian Institute of Science

2015

Investigations on supersonic flows in miniature shock tubes.

Janardhanraj Subburaj, Indian Institute of Science

2015

Studies on impinging shock wave Boundary Layer Interactions.

Sriram R, Indian Institute of Science

2014

Studies on supersonic gaseous ejector

Srisha Rao, Indian Institute of Science

2009

Effect of shock waves on pathogenic infection

Divya Prakash G, Indian Institute of Science

2009

Demonstration of supersonic combustion in a combustion driven shock-tunnel.

Ratan Joarder, Indian Institute of Science

2008

Investigations of Ramp/Cowl Shock Interaction Processes near a generic SCRAMJET inlet at Hypersonic Mach number.

Debabrata Mahapatra, Indian Institute of Science

2007

Shock tunnel investigations on hypersonic separated flows.

Reddeppa P, Indian Institute of Science

2007

The effect of Energy deposition in Hypersonic blunt body flow field.

Satheesh K, Indian Institute of Science

2007

Experimental Investigation Of The Effect Of Nose Cavity On The Aerothermodynamics Of The Missile Shaped Bodies Flying At Hypersonic Mach Numbers.

Saravanan S, Indian Institute of Science

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