Shashi Bhushan Verma
VIDWAN ID: 66489

Dr Shashi Bhushan Verma

Male Doctor of Philosophy
Chief Scientist | Experimental Aerodynamics Division
CSIR-National Aerospace Laboratories
Karnataka
Expertise: Aerospace Engineering
110 Publications
0 Projects
1425 Scopus Citations
1230 CrossRef
22 Years 8 Months Total Experience
Publications
110 Total
Articles
80
Proceedings
30
Activity

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Scopus Scopus
1,425 Citations
22 h-index
CrossRef CrossRef
1,230 Citations
22 h-index
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Personal Details

Doctor of Philosophy
N/A
Chief Scientist
Feb 2019 – Present
CSIR-National Aerospace Laboratories | Experimental Aerodynamics Division
Principal Scientist
Jan 2004 – Feb 2019
CSIR-National Aerospace Laboratories | Experimental Aerodynamics Division
Engineering and Technology
Aerospace Engineering

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Scholarly Work

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Scholarly Publications

Cold gas dual-bell tests in high-altitude simulation chamber

Journal Article
Shock Waves. Year: 2011. Volume: 21 , Issue: 2 , Pages: 131-140 .
Authors: S. B. Verma; R. Stark; C. Génin; O. Haidn

Cold gas testing of thrust-optimized parabolic nozzle in a high-altitude test facility

Journal Article
Journal of Propulsion and Power. Year: 2011. Volume: 27 , Issue: 6 , Pages: 1238-1246 .
Authors: S.B. Verma; Oskar Haidn

Study of jets from rectangular nozzles with square grooves

Journal Article
Year: 2011. Volume: 115 , Issue: 1165 , Pages: 187-196 .
Authors: P. Arun Kumar; S. B. Verma; S. Elangovan

Shockwave/boundary-layer interaction control on a compression ramp using steady microjets

Journal Article
AIAA Journal. Year: 2012. Volume: 50 , Issue: 12 , Pages: 2753-2764 .
Authors: S. B. Verma; C. Manisankar

An experimental study of subsonic and sonic jets controlled by air-tabs

Conference Paper
Year: 2015.

Studies on the influence of steady microactuators on shock-wave/boundary- layer interaction

Conference Paper
AIAA Journal. Year: 2013. Volume: 51 , Issue: 12 , Pages: 2753-2762 .
Authors: Mohd Y. Ali; Farrukh S. Alvi; Rajan Kumar; C. Manisankar; S. B. Verma; L. Venkatakrishnan

Effect of spike truncation on the acoustic behavior of annular aerospike nozzles

Conference Paper
AIAA Journal. Year: 2013. Volume: 51 , Issue: 9 , Pages: 2168-2182 .
Authors: N. Karthikeyan; Ashwin Kumar; S. B. Verma; L. Venkatakrishnan

Origin of flow asymmetry in planar nozzles with separation

Journal Article
Shock Waves. Year: 2014. Volume: 24 , Issue: 2 , Pages: 191-209 .
Authors: S. B. Verma; C. Manisankar
Showing 49 to 56 of 110 publications