Prof B T N Sridhar
vidwan id: 117672
Professor, Department of Aerospace Engineering
Anna University
Expertise
- Aerospace Engineering
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Scopus
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14
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Citations
398
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12
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Community & Membership
Syllabus Subcommittee for B.E. Aeronautical Engineering, Anna University
MemberSyllabus Subcommittee for B.E. Aerospace Engineering, Anna University
MemberAnti Ragging Committee, MIT Campus, Anna University
MemberIndian Society of Systems for Science and Engineering
High Energy Materials society of India
Aeronautical Society of India
Bio
High Speed Jets and Propulsion
Personal Details
- Male
- Professor , Anna University
- Department of Aerospace Engineering, Anna University
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Co-Authors (14)
Anna University
Bharath Institute of Higher Education & Research
Anna University
Anna University
Institute of Aeronautical Engineering
Prof Mahendra Perumal Govindan
S R M Institute of Science & Technology, Chennai
B S Abdur Rahman Crescent Institute of Science & Technology, Kancheepuram
Indian Institute of Technology Madras
Vel Tech Rangarajan Dr. Sagunthala R & D Institute of Science & Technology, Chennai
Anna University
Indian Institute of Technology Madras
Bharath Institute of Higher Education & Research
N/A
Scholarly Work
Impact Characterization of Laminate Composites
Funding Agency: ADE
Principal Investigator
985,000
2010 - 2012
Development of Reaction Control Systems using Solid Hot Gas Generators
Funding Agency: RCI
Principal Investigator
784,000
2009 - 2012
Development of Gas Generator formulations with Low Flame Temperature
Funding Agency: RCI
Principal Investigator
980,000
2005 - 2008
Tip to End Flow Simulation of HSTDV Configuration Incorporating Pylon Based Scramjet Combustor
Funding Agency: DRDL
Principal Investigator
984,000
2004 - 2006
Experimental Evaluation of Component Characteristics of HRV at Low Speeds
Funding Agency: DRDL
Coinvestigator
194,400
2003 - 2005
Estimation of Control Characteristics of HRV at Low Speeds
Funding Agency: DRDL
Coinvestigator
198,000
2003 - 2005
Mathematical Modelling of Flow in a Kerosene Fuelled Scramjet Combustor
Funding Agency: DRDL
Principal Investigator
495,000
2001 - 2004
Experimental Evaluation of Aerodynamic Characteristics of HRV vehicle configuration at Low speeds
Funding Agency: DRDL
Principal Investigator
448,500
2001 - 2004
Combustion Characteristics of AP-HTNR Composite Solid Propellants and HTNR Polymer
Funding Agency: AICTE
Coinvestigator
500,000
1996 - 2000
Effect of Burning Rate Modifiers on Surface Temperature of Composite solid Propellants
Funding Agency: University Grants Commission, New Delhi, India
Coinvestigator
500,000
1992 - 1996
Mechanical and Ballistic Behavioural Study of HTPB based Composite Solid Propellants
Incompressible Flow Over Elliptic Cones With Base Jets
Effects of Geometric Configuration and Velocity Ratio on the Near Field Flow Characteristics of Coaxial Jets: An Experimental Study
An Experimental Study on Effect of Inner Jet shapes On the Mixing Characteristics of High Speed Coaxial Jets
Thermal Analysis of HTPB-Paraffin Blends for Aerospace Applications
Characterization and Development of Gas Generator Propellant
Shock Cell Structure, Decay and Spread Characteristics of Noncircular Supersonic Jets
Experimental Studies on the Effect of Groove Shapes On supersonic Jets Issuing From Circular and Elliptical Nozzles
Effect of Diagonal Expansion Ramps On Mixing and Noise Characteristics of Supersonic Rectangular Jet
Experimental Study of Flow Characteristics of Non Circular Supersonic Jets in the Presence of an Annular Coflow at Large Separation Distance
Experimental Study of Strut Insertion Through Divergent Wall of A Convergent-Divergent Nozzle for Thrust Vector Control
Experimental Studies on Interaction of a Supersonic Flow with a Strut Placed on an Expansion Ramp
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Scholarly Publications
Experimental analysis of non circular co-flow in the incompressible coaxial jets
Open AccessAn experimental study on comparison of non-circular co-flow jet with co-axial jets and computational verification
Open AccessUltimate Strength Prediction of Carbon/Epoxy Tensile Specimens from Acoustic Emission Data
Open AccessExperimental study on ballistic behaviour of an aluminised AP/HTPB propellant during accelerated aging
Open AccessCorrelation of dielectric permittivity with mechanical properties in soft tissue-mimicking polyacrylamide phantoms
Open AccessCorrelation of electrical impedance with mechanical properties in models of tissue mimicking phantoms
Open AccessExperimental evaluation and simulation on aging characteristics of aluminised AP-HTPB composite solid propellant
Open Access
10.1179/174328408X278420
19
26