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Dr Shashi Bhushan Verma

vidwan id: 66489
Male

Chief Scientist, Experimental Aerodynamics Division
CSIR-National Aerospace Laboratories

Expertise

  • Aerospace Engineering

Publications

Total Articles 98
Books 0
Proceedings 0

Publications

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Scopus

Citations 742
h-index 15

CrossRef

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Citations 661
h-index 15
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Bio

Dr. Verma’s research interests are in the study of flow separation in subsonic, transonic, and supersonic regimes and in developing appropriate flow control technologies to alleviate their adverse effects. In particular, the focus areas include flow separation associated side-load development in liquid rocket engine nozzles before launch vehicle lift-off, shock-induced supersonic and transonic Interactions related to air-intakes and, afterbody flows and freestream-jet interactions related to pro

Personal Details

  • Male
  • Chief Scientist , CSIR-National Aerospace Laboratories
  • CSIR - National Aerospace Laboratories
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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

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Co-Authors (11)

Ajay

Prof Ajay Misra

Vidyasagar University

Jayaprakash Narayan

Dr Jayaprakash Narayan Murugan

Vellore Institute of Technology, Vellore

Kiran

Dr Kiran Chutkey

CSIR-National Aerospace Laboratories

Manishankar

Dr Manishankar C

CSIR-National Aerospace Laboratories

Viji

Mr Viji M

CSIR-National Aerospace Laboratories

S

Dr S Sudhakar

Central Electrochemical Research Institute

Sudhakar

Mr Sudhakar Senthamarai

CSIR-National Aerospace Laboratories

L

Dr L Venkatakrishnan

CSIR-National Aerospace Laboratories

Vikramaditya

Dr Vikramaditya N.S

CSIR-National Aerospace Laboratories

Scholarly Work

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Scholarly Publications

Effect of Passive Flow Control Devices on Base Pressure for Mach Numbers Between 0.5 and 1.4

Open Access
Article
Authors: Murugan J.N.;Chutkey K.;Sri Raghu R.;Verma S.B.

Assessment of Flow Field Behind the Mechanical Vortex Generators at Mach 2.0

Open Access
Conference Paper

Off- And on-surface studies on flow development from various vortex generators configurations at Mach 2.0

Open Access
Article
Authors: Chidambaranathan M.;Singh I.;Narayanan S.;Verma S.B.

Effect of throttling on dual-bell sneak-transition side loads

Open Access
Article

Topological modifications due to ramped vanes in a flare-induced shock–boundary layer interaction flowfield

Open Access
Article

Unsteady side-load evolution in a liquid rocket engine nozzle

Open Access
Note

Shock-induced flow separation in an overexpanded supersonic planar nozzle

Open Access
Article

An experimental investigation of turbo-ramjet engine intake at mach 4

Open Access
Conference Paper
Authors: Raju N.;Pai T.G.;Verma S.B.;Venkatakrishnan L.