Ministry of Education
Vidvan Image

Ms Shobhavathy M.T

vidwan id: 69219
Female

Senior Principal Scientist, Propulsion Division
CSIR-National Aerospace Laboratories

Google Scholar Icon 56078630900

Expertise

  • Aerospace Engineering

Publications

Total Articles 16
Books 0
Proceedings 0

Publications

No publication activity to display at the moment.

Scopus

Citations 155
h-index 7

CrossRef

CrossRef Icon
Citations 91
h-index 5
Google Scholar

Loading Scholar statistics...

Professional Recognition

No Data Found

There is currently nothing to display here.

Community & Membership

No Data Found

There is currently nothing to display here.

No Data Found

There is currently nothing to display here.

Bio

Heat Power Engineering

Personal Details

  • Female
  • Senior Principal Scientist , CSIR-National Aerospace Laboratories
  • CSIR-National Aerospace Laboratories
No Data Found

There is currently nothing to display here.

Senior Principal Scientist Aug 2015 – Present
CSIR-National Aerospace Laboratories | Propulsion Division
Principal Scientist Aug 1994 – Aug 2015
CSIR-National Aerospace Laboratories | Propulsion Division

Related Profiles

Experts (989+)

View All
Pragati

Ms Pragati Mishra

Assistant Professor

Sridhar

Dr Sridhar Sekar

Assistant Professor

DEEPAK

Mr DEEPAK B N

N/A

Md

Dr Md Nadeem M

Assistant Professor

Rashmi

Rashmi Chandra

Assistant Professor

Anjali

Dr Anjali Jadhav

Doctor

Abhishek

Mr Abhishek Shukla

Assistant Professor (Grade-I)

N

Dr N PRAKASH

Assistant Professor

Mrinmoy

Mr Mrinmoy Sadhukhan

Research Scholar

Haranath

Mr Haranath Rakshit

Junior Research Fellow

Organisations (387+)

View All
Ashoka

Mr Ashoka B.S

Technical Officer

Buddhadeb

Mr Buddhadeb Nath

Scientist

Balaji

Mr Balaji S

Principal Scientist

Aruna

Dr Aruna S T

Senior Principal Scientist

Arun

Mr Arun Kumar,A

Scientist

Arun

Mr Arun S

Scientist

Udayakumar

Dr Udayakumar A

Senior Principal Scientist

K.N.

Mr K.N. Arunkumar

Chief Scientist

Arvind Kumar

Shree Arvind Kumar Yadav

Scientist

Selvamani

Mr Selvamani Babu,A.S

Principal Technical Officer

Co-Authors (8)

A M

Dr A M Pradeep

Indian Institute of Technology Bombay

Avinash Kumar

Mr Avinash Kumar R

PSG INSTITUTE OF TECHNOLOGY AND APPLIED RESEARCH

Dileepkumar

Dr Dileepkumar Bhanudasji Alone

CSIR-National Aerospace Laboratories

Ranjan

Prof Ranjan Ganguli

Indian Institute of Science Bangalore

S. B.

Dr S. B. Kandagal

Indian Institute of Science Bangalore

Lakshya

Mr Lakshya Kumar

CSIR-National Aerospace Laboratories

Senthil Kumaran

Mr Senthil Kumaran Raju

CSIR-National Aerospace Laboratories

Venkat Iyengar

Dr Venkat Iyengar S

CSIR-National Aerospace Laboratories

Scholarly Work

No Data Found

There is currently nothing to display here.

No Data Found

There is currently nothing to display here.

No Data Found

There is currently nothing to display here.

Scholarly Publications

Aeroelastic Aspects of Axial Compressor Stage With Self-Recirculating Casing Treatment

Open Access
Article
Journal of Turbomachinery. Year: 2022. Volume: 144 , Issue: 6 .
Authors: Satish Kumar S.;Alone D.B.;Thimmaiah S.M.;Mudipalli J.R.R.;Kumar L.;Jana S.;Kandagal S.B.;Ganguli R.
DOI 10.1115/1.4053385
9 13

Aerodynamic behavior of a transonic axial flow compressor stage with self-recirculating casing treatment

Open Access
Article
Aerospace Science and Technology. Year: 2021. Volume: 112 .
Authors: Kumar S.S.;Bhanudasji Alone D.;Thimmaiah S.M.;Mudipalli J.R.R.;Kumar L.;Ganguli R.;Kandagal S.B.;Jana S.
DOI 10.1016/j.ast.2021.106587
31 36

Design of high transonic axial compressor stage for small gas turbine applications

Open Access
Conference Paper
Year: 2019. Volume: 1 .
Authors: Satish Kumar S.;Kumar L.;Senthil Kumaran R.;Kumar V.S.;Shobhavathy M.T.
DOI 10.1115/GTINDIA2019-2690

A CFD analysis to study the effect of vortex generator on axial compressor performance

Open Access
Article
Year: 2019. Volume: 9 , Issue: Special Issue 2 , Pages: 868-876 .
Authors: Adarsh B.G.;Shobhavathy M.T.;Ajithkumar R.

Aerodynamic characterization of a transonic axial flow compressor stage – with asymmetric tip clearance effects

Open Access
Article
Aerospace Science and Technology. Year: 2018. Volume: 82-83 , Pages: 272-283 .
Authors: Kumar S.S.;Bhanudasji Alone D.;Thimmaiah S.M.;Mudipalli J.R.R.;Ganguli R.;Kandagal S.B.;Jana S.
DOI 10.1016/j.ast.2018.09.001
20 29

Experimental assessment on effect of lower porosities of bend skewed casing treatment on the performance of high speed compressor stage with tip critical rotor characteristics

Open Access
Article
Aerospace Science and Technology. Year: 2017. Volume: 60 , Pages: 193-202 .
Authors: Alone D.B.;Kumar S.S.;Shobhavathy M.T.;Mudipalli J.R.R.;Pradeep A.M.;Ramamurthy S.;Iyengar V.S.
DOI 10.1016/j.ast.2016.11.006
13 28

Stability management of high speed axial flow compressor stage through axial extensions of bend skewed casing treatment

Open Access
Article
Propulsion and Power Research. Year: 2016. Volume: 5 , Issue: 3 , Pages: 236-249 .
Authors: Alone D.B.;Kumar S.S.;Thimmaiah S.M.;Mudipalli J.R.R.;Pradeep A.M.;Ramamurthy S.;Iyengar V.S.
DOI 10.1016/j.jppr.2016.01.009
5 14

CFD analysis to investigate the effect of vortex generators on a transonic axial flow compressor stage

Open Access
Conference Paper
Year: 2015.
Authors: Rajendran A.K.;Shobhavathy M.T.;Kumar R.A.
DOI 10.1115/GTINDIA2015-1313
5