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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

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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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Organisations (387+)

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Principal Scientist

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Senior Principal Scientist

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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

Influence of base cavity on base pressure at subsonic and supersonic Mach numbers

Open Access
Conference Paper

Study of vortex breakdown and pitch up on a compound delta wing

Open Access
Article

Control of compression-ramp-induced interaction with steady microjets

Open Access
Article

Control of incident shock-induced boundary-layer separation using steady micro-jet actuators at M∞ = 3.5

Open Access
Article
Authors: Chidambaranathan M.;Verma S.B.;Rathakrishnan E.

Control of incident shock-induced separation using vane-type vortex-generating devices

Open Access
Article

Effect of cross wire tab orientation on twin jet mixing characteristics

Open Access
Article

Analysis of shock unsteadiness in a supersonic over-expanded planar nozzle

Open Access
Article
Authors: Verma S.;Chidambaranathan M.;Hadjadj A.

Interaction of external flow with linear cluster plug nozzle jet

Open Access
Article