Ministry of Education
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Mr Nagashetty K

vidwan id: 240127
Male

Scientific Officer, Aerospace Engineering
Indian Institute of Science Bangalore

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Expertise

  • Aerospace Engineering

Publications

Total Articles 14
Books 0
Proceedings 0

Publications

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Scopus

Citations 130
h-index 7

CrossRef

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Citations 80
h-index 6
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Bio

Aerodynamics and Shock Wave dynamics

Personal Details

  • Male
  • Scientific Officer , Indian Institute of Science Bangalore
  • Indian Institute of Science
M.Sc
Other Institute 2015
B.E
Bangalore University 1998
Scientific Officer Apr 1980 – Present
Indian Institute of Science Bangalore | Aerospace Engineering

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Co-Authors (4)

Gopalan

Prof Gopalan Jagadeesh

Indian Institute of Science Bangalore

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Prof K. P. J. Reddy

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Dr Sriram Rengarajan

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Scholarly Work

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Scholarly Publications

Heat transfer measurements on waverider at hypersonic mach numbers

Open Access
Conference Paper
Year: 2014.
Authors: Nagashetty K.;Siram R.;Saravanan S.;Jagadeesh G.;Reddy K.P.J.
1 1

Measurement of heat transfer rate on backward-facing steps at hypersonic mach number

Open Access
Article
Journal of Thermophysics and Heat Transfer. Year: 2011. Volume: 25 , Issue: 3 , Pages: 321-328 .
Authors: Reddeppa P.;Nagashetty K.;Saravanan S.;Jagadeesh G.;Gai S.L.
DOI 10.2514/1.47101
13 18

Schlieren visualization of shock wave phenomena over a missile-shaped body at hypersonic Mach numbers

Open Access
Article
Year: 2011. Volume: 225 , Issue: 1 , Pages: 26-34 .
Authors: Saravanan S.;Nagashetty K.;Hegde G.M.;Jagadeesh G.;Reddy K.P.J.
DOI 10.1243/09544100JAERO827
8 10

Experimental investigations on the effect of a thermal bump in the hypersonic flow around a flat plate

Open Access
Conference Paper
Year: 2009.
Authors: Jagadeesh G.;Sriram R.;Hariharan M.S.;Saravanan S.;Nagashetty K.;Reddy K.P.J.
DOI 10.2514/6.2009-1402
2 4

Studies on the effects of test gas on the flow field around large angle blunt cone flying at hypersonic mach number

Open Access
Article
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. Year: 2002. Volume: 45 , Issue: 149 , Pages: 189-194 .
Authors: Jagadeesh G.;Nagashetty K.;Reddy K.;Sun M.;Takayama K.
DOI 10.2322/tjsass.45.189
2 4

Experimental investigations of test gas effects on the hypersonic flow field around large angle blunt cone in shock tunnel

Open Access
Conference Paper
Year: 2001.
Authors: Jagadeesh G.;Sun M.;Nagashetty K.;Reddy K.R.J.
DOI 10.2514/6.2001-305
3 2

Gas temperature layer visualization in hypersonic shock tunnel using electric discharge

Open Access
Conference Paper
Year: 2001. Volume: 4183 , Pages: 864-871 .
Authors: Jagadeesh G.;Nagashetty K.;Srinivasa Rao B.;Reddy K.
DOI 10.1117/12.424246

Shock stand-off distance visualization in hypersonic shock tunnel using electrical discharge technique

Open Access
Article
Year: 2001. Volume: 4183 , Issue: 1 , Pages: 674-681 .
Authors: Nagashetty K.;Syed Saifuddin K.;Saravanan S.;Gurumurthy K.;Reddy K.
DOI 10.1117/12.424341
1 1