Ministry of Education
C Senthil Kumar
VIDWAN ID: 117669

Prof C Senthil Kumar

Male Doctor of Philosophy
Professor | Department of Aerospace Engineering
Anna University, Chennai (2017)
Tamil Nadu
Expertise: Aerospace Engineering
ORCID 0000-0002-6908-2249 Scopus 53875938500 ResearcherID AGH-2728-2022 Google Scholar 8NsZ2uoAAAAJ
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22 Publications
9 Projects
87 Scopus Citations
47 CrossRef
23 Years Total Experience
Publications
22 Total
Articles
15
Proceedings
7
Activity

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Scopus Scopus
87 Citations
5 h-index
CrossRef CrossRef
47 Citations
4 h-index
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Professional Recognition

Best Paper
2012
NIT Rourkela-769 008

Community & Membership

Result Passing Board of Kongu Engineering College, Erode
University Representative and member
Nov 2021 – May 2022
Aerodynamic Design of STAR vehicle
Review member
Oct 2019
Long Range Glide Bomb
Member of Preliminary Design Review
Nov 2018
Aeronautics Research Development Board - Aerodynamics Panel (DRDO)
Member
Jan 2022
Aeronautical Society of India - Chennai Branch
Chairman
Jan 2023
Board of Studies in Manufacturing, Annamalai University
Member
Feb 2024
Indian Society for Technical Education
Life Member
Jan 1996
Aeronautical Society of India
Fellow
Jan 2024
High Energy Material Society of India
Life Member
Jan 2004
Institution of Engineers
Fellow
Jan 2023

Personal Details

Doctor of Philosophy
2009
N/A
Master of Engineering
1995
Sultan Qaboos University, Muscat
Bachelor of Engineering
1993
BABU BANARASI DAS INSTITUTE OF TECHNOLOGY AND MANAGEMENT, LUCKNOW
Professor
May 2017 – —
Anna University, Chennai | Department of Aerospace Engineering
Associate Professor
May 2014 – Apr 2017
Anna University, Chennai | Department of Aerospace Engineering
Assistant Professor
Aug 2001 – Apr 2014
Anna University, Chennai | Department of Aerospace Engineering
Lecturer - Senior Scale
Feb 1997 – Jul 2001
Bannari Amman Institute of Technology
Lecturer
May 1995 – Feb 1997
Adiyaman College of Engineering
Engineering and Technology
Aerospace Engineering

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Scholarly Work

Passive Method of Base Drag Reduction for Range Enhancement of Gun Launched Shell Configuration
Completed
Agency: Defence Research and Development Organisation Role: Principal Investigator
Amount: ₹53.36 Lac
Duration: 2017 – 2019
Evaluation of Stall Characteristics of Wing & Control Surface and Overall Characteristics of a Typical Missile Configuration
Completed
Role: Principal Investigator
Amount: ₹14.87 Lac
Duration: 2016 – 2017
Evaluation of Stall Characteristics of the Control Surface of RCI Reduced Dimension Vehicle
Completed
Agency: Defence Research and Development Organisation Role: Principal Investigator
Amount: ₹7.07 Lac
Duration: 2015 – 2015
Setting up of Combustion Driven Shock Tunnel
Completed
Role: Principal Investigator
Amount: ₹44.06 Lac
Duration: 2014 – 2016
Development of Mathematical Model for Prediction of Energy Loss in Canister during Missile Launching
Completed
Role: Principal Investigator
Amount: ₹24.98 Lac
Duration: 2014 – 2016
Thermal Characterisation and Analysis of C/C Samples for Aerospace Application
Completed
Role: Co-Principal Investigator
Amount: ₹8.39 Lac
Duration: 2014 – 2016
Calibration of Orifice Plates at Different Air Flow Rates Using the Air Blower
Completed
Role: Principal Investigator
Amount: ₹35,294
Duration: 2014 – 2014
Force measurements for the UAV model using our Wind tunnel and 6-componet internal balance
Completed
Role: Principal Investigator
Amount: ₹2.27 Lac
Duration: 2013 – 2013
Model Mounting and Attitude Change Mechanism for the Low Speed Wind Tunnel at MIT
Completed
Role: Principal Investigator
Amount: ₹19.16 Lac
Duration: 2008 – 2011

Studies of Winglet Effect on Lift Induced Drag in Aircraft Model

University MIT Campus, Anna University
Year 2015
Downloads 0

Optimization Of Oil-Cooler Duct Location For A Pusher Type Turboprop Aircraft

University MIT Campus, Anna University
Year 2017
Downloads 0

Improvements Of Wind Turbine Performance Using Boundary Layer Fence

University MIT Campus, Anna University
Year 2017
Downloads 0

Investigation of Fore Body Geometrical Effects on Drag and Flow Field of D-Shaped Model

University MIT Campus, Anna University
Year 2019
Downloads 0

Experimental Investigation of Downstream Flow Characteristics of Circular And Square Towers With Different Taper Ratios

University MIT Campus, Anna University
Year 2019
Downloads 0

Investigation of surface pressure distribution and heat flux on Re-entry vehicle using shock tunnel

University MIT Campus, Anna University
Year 2019
Downloads 0

Jet flow control using semi-circular corrugated tabs

University MIT Campus, Anna University
Year 2019
Downloads 0

Tower Shadow And Wind Pressure Characteristics Of Horizontal Axis Wind Turbine Tower Systems

University MIT Campus, Anna University
Year 2020
Downloads 0

Acoustic Pressure Oscillation Effects on Mean Burning Rate of Solid Propellant

University MIT Campus, Anna University
Year 2020
Downloads 0

Base Drag Reduction Using Inward-Turning Base Bleed in Shell Projectile

Chairman
DRDO
New Delhi & The Registrar
Anna University
Chennai
- Application No. : 202211047345 Filed : 19-08-2022
Published : 25-10-2024 Published

Saw toothed leading edge delta wings

Anna University
- Patent No. : 459345 Filed : 31-05-2016
Published : 10-06-2016 Granted

Sinusoidal toothed leading edge delta wings

Anna University
- Patent No. : 529447 Filed : 31-05-2016
Published : 10-06-2016 Granted

Scholarly Publications

Development of an algorithm for dynamic grid generation

Conference Paper
Year: 2007.
Authors: G. Aswin; M. Kalaiselvan; C. Senthil Kumar; S. Elangovan
DOI 10.4271/2007-01-1401

Influence of Boundary Layer control on wind turbine blade aerodynamic characteristics – Part I – Computational study

Conference Paper
Year: 2013. Pages: 1211-1217 .
Authors: T. A. Sundaravadivel; S. Nadaraja Pillai; C. Senthil Kumar
DOI 10.3850/978-981-07-8012-8_211 Crossref Crossref: 1 Scopus Scopus: 5

Experimental analysis on a wind turbine model with a 3-D span wise projection for passive flow control

Conference Paper
Year: 2013. Pages: 1263-1268 .
Authors: T. A. Sundaravadivel; S. Nadaraja Pillai; C. Senthil Kumar
DOI 10.3850/978-981-07-8012-8_277 Scopus Scopus: 2

Effect of pitch angle on blade - Tower interference on HAWT

Conference Paper
Year: 2013. Pages: 1172-1177 .
Authors: N. I. Haroon Rashid; S. Nadaraja Pillai; C. Senthil Kumar
DOI 10.3850/978-981-07-8012-8_158

Pressure, force and moment measurements on aircraft model at subsonic wind tunnel

Journal Article
Year: 2014. Volume: 9 , Issue: 24 , Pages: 28555-28562 .

Wind tunnel investigation of downstream wake characteristics on circular cylinder with various taper ratios

Open Access
Journal Article
Journal of Applied Fluid Mechanics. Year: 2017. Volume: 10 , Issue: SpecialIssue , Pages: 69-77 .
DOI 10.36884/jafm.10.SI.28272 Crossref Crossref: 2 Scopus Scopus: 22

Investigation of Engine Oil-cooling Problem during Idle Conditions on Pusher Type Turbo Prop Aircraft

Journal Article
Year: 2017. Volume: 34 , Issue: 4 , Pages: 333-340 .
Authors: P. S. Premkumar; S. Bhaskar Chakravarthy; S. Jayagopal; P. Radhakrishnan; S. Nadaraja Pillai; C. Senthil Kumar
DOI 10.1515/tjj-2016-0013 Crossref Crossref: 1 Scopus Scopus: 3

Experimental Investigation on Drag Characteristics of HAWT Tower Due to Tower Shadow

Journal Article
Year: 2018. Volume: 39 , Issue: 1 , Pages: 105-111 .
Scopus Scopus: 1
Showing 1 to 8 of 22 publications