Introduction

The Propulsion Panel was constituted in 1972 with objectives to sponsor research , development and design projects in the field of Aircraft Propulsion, keeping in view the future needs of the country with regard to the development of aero-gas turbine engine for military applications. Subsequently, the panel has widened its scope of activities to cover frontier areas in aerospace propulsion and to address problems related to civil aviation.

Panel Activities

The Propulsion Panel was constituted by the AR&DB with following objectives:

To promote research and development activities related to aero-gas turbine engine and rocket propulsion. To support projects directly or indirectly related to the indigenous gas turbine engine program. Also to support basic and fundamental projects on all aspects of aircraft and rocket propulsion being undertaken at the Institutes of higher learning. The Panel has also initiated some projects related to civil aviation. The following types of project have been promoted through the Panel:

  • Applied research and development projects whose outcome has a promising application as a retrofit to the engines, manufactured under license or in the new engine under consideration for development.
  • Demonstration of a new/advanced concept or a measurement technique under simulated conditions of promising application in gas turbine engines/ propulsion systems.
  • Generation of general purpose design data through parametric investigation and or validation of general purpose computerized design/ analysis methods experimental design data.
  • Fundamental investigation to understand in depth the behavior of components/ systems and evolve a scientific basis for the explanation of their behavior, as a pursuit of knowledge related to the propulsion field.

Panel Members

Dr V Ramanujachari
CSIR-Bhatnagar-Fellow

Official Address :
National Centre for Combustion Research and Development (NCCRD), IIT Madras, Chennai- 600036.

Office : 044-22579881
E-mail :vramanujachari[at]yahoo[dot]co[dot]in

C/MCoordinator

Panel Members
Sr. No.Member NameDesignationOfficial AddressTele/FaxC/M
1Dr V RamanujachariCSIR-Bhatnagar-FellowNational Centre for Combustion Research & Development (NCCRD), IIT Madras, Chennai-600036vramanujachari[at]yahoo[dot]co[dot]inCoordinator
2Dr RV Ravi KrishnanProfessorDepartment of Mech. Engineering, IISc, Bangalore-560012ravikris[at]mecheng[dot]iisc[dot]ernet[dot]inMember
3Dr SR ChakravarthyProfessorDepartment of Aerospace Engineering, IIT, Madras044-22574011 (O)
044-22574002 (Fax)
src[at]ae[dot]iitm[dot]ac[dot]in
Member
4Dr Debasis ChakrabortyScientist GProject Director, HSTDV, DRDL, Hyderabad040-24583310 (O)
040-24345325 (Fax)
debasis_cfd[at]drdl[dot]drdo[dot]in
Member
5Dr Abhijit KushariProfessorDepartment of Aerospace Engineering, IIT, Kanpur-208016akushari[at]iitk[dot]ac[dot]inMember
6Dr K Nanda KumarHead, CRD/ PRSGLiquid Propulsion Systems Centre (LPSC), Valiamala, Trivandrum-6955470471-2567794 (O)
0471-2567094 (Fax)
nandakumar_k1[at]yahoo[dot]com
Member
7Dr AK DarpeProfessorDeptt. of Mechanical Engg., IIT, Delhi011-26596095
011-26582053 (Fax)
akdarpe[at]mech[dot]iitd[dot]ac[dot]in
Member
8Shri KM Unni(Retd.)Dir-EngineeringAir India, Santacruz Airport, Mumbai- 400029022-26157020
022-26157068 (Fax)
km[dot]unni[at]airindia[dot]in
Member
9Shri RK MishraScientist FRCMA (Engines), CEMILAC, Marathahalli Colony Post, Bangalore - 560 037080-25241488
080-25240075 (Fax)
rkmishra[dot]drdo[at]gmail[dot]com
Member
10Shri H SiddeshaScientist GProject Director (PS), ADA, Bangalore080-25238493
080-25238579 (Fax)
siddesha[at]jetmail[dot]ada[dot]gov[dot]in
Member
11Dr R RajendranPrinciple Scientist & Dy Head Propulsion DivisionNational Aerospace Laboratory, Bangalore080-25081787/1788
080-25222494 (Fax)
rrajendran[at]nal[dot]res[dot]in
Member
12Shri RaghvendraScientist 'E'Aeronautical Development Establishment, CV Raman Nagar PO, Bangalore-560093080-25057152
lnraghav[at]ade[dot]drdo[dot]in
Member
13Dr Maitreyee NandaSecy. AR&DBAR&DB Sectt., 'A' Wing, DRDO Bhawan, Rajaji Marg, New Delhi-110011Tel: 011-23007803
Fax: 011-23007853
mnanda[at]hqr[dot]drdo[dot]in
ardb[at]hqr[dot]drdo[dot]in
Member Secy

Projects

Projects
Project TitlePrincipal InvestigatorInstitute
Orpheus 703R-2000K.AVM S N RoychowdhuryGTRE, Bangalore
Research on GTX-Engine components.AVM S N RoychowdhuryGTRE, Bangalore
Design condtruction and commissioning of a cascade wind tunnel.Prof. S SoundaranayagIISc, Bangalore
Boundary layer development in compressor and turbine cascades.Prof. S SoundaranayagIISc, Bangalore
To carry out simulated flight performance testing of the 703-R-2000 degree K reheat system in high altitude test beds.AVM S N RoychowdhuryGTRE, Bangalore
Influence of slot geometery and free stream turbulance on the cooling efffectiveness of film cooled turbine.Dr. W V NabarIIT, Bombay
Investigation of high speed rotor vibration.Dr. S K SaneIIT, Bombay
Investigation of blade vibration.Dr. S K SaneIIT, Bombay
Investigation of blade vibration.Dr. B S ChittawadgiIIT, Bombay
Investigation of heat transfer to turbine nozzle blade with heat resistant coating.Dr. W V NabarIIT, Bombay
Effect of surface finish and porosity on heat transfer in a compressible flow with arbitrary pressur egradient.Dr. S K SaneIIT, Bombay
Design and performance testing of turbine blades cascade suitable for supersonic inlet velocities.Dr. S K SaneIIT, Bombay
Feasibility study on use of ex-service aircraft engine as power plant in military and civil applications.Dr. S K SaneIIT, Bombay
Investigation in exhaust pollutant of aircraft turbojet engine and investigation in the performance of a full scale main.Dr. B S ChittawadgiIIT, Bombay
Investigation of thermodynamic processes of aircraft gas turbine engine under.Dr. S K SaneIIT, Bombay
To prepare a flexible and accurate calculation procedure and necessary computer programme for performance.Dr. B S ChittawadgiIIT, Bombay
Investigation of heat transfer to the impulse rotor blades at supersonic velocities.Dr. S K SaneIIT, Bombay
Prediction & measurement of air pollutants found in gas turbine combustion chamber.Dr. B S ChittawadgiIIT, Bombay
Theoretical & experimental investigation in estimation of true thermodynamics efficiencies of compressor turbine.Dr. S K SaneIIT, Bombay
Research on hybrid rockets.Prof. A K ChatterjiBIT, Ranchi
Hypergolic ignition studies with N2O4 and RRNA oxidiser.Prof. B L GuptaBIT, Ranchi
Ignition delay variation in hypergolic propellants under reduced ambient pressure and temperatures.Prof. S N AgarwalBIT, Ranchi
Two dimensional and annular cascade studies on JT-3D engine compressor and turbine blade.Dr. R SinghIIT, Kanpur
Two dimensional flow in axial turbomachine.Dr. R SinghIIT, Kanpur
Experimenta; and theoritical study of blade vibrations.Dr. N G R IyengarIIT, Kanpur
Flow properites behind flame stabliser symmetric and assymmetric configuration.Dr. A K GuptaIIT, Kanpur
Rocket combustion and flow through rocket nozzles.Dr. O P SharmaIIT, Kanpur
High speed cascade tests.Prof. D PrithvirajIIT, Madras
High speed compressor and turbine investigation.Prof. D PrithivirajIIT, Madras
Design & developemnt of ramjet engine.Dr. K DamodharanIIT, Madras
Effect of variable starters on performance of multistage axial compressor.Dr. S SoudranayagamIISc, Bangalore
Research on high temperature combustion chamber for small gas turbine.Prof. B C DuttaIISc, Bangalore
Hybrid rocket motor.Dr. V K JainIISc, Bangalore
Some studies on composite solid propellant rocket.Dr. V K JainIISc, Bangalore
Combustion studies on composite solid propellant rocket.Dr. H L GirdharKashmir Univ
Theoretical study of the effect of swirling motion on flame characteristics.Dr. O P SharmaIIT, Kanpur
Contrl of ignition of propellants.Dr. T P PandyaLucknow Univ
Study of jet noise.Sh. C K GroverRoorkee Univ
Drilling of long sleder holes in high strength temperature resistant metals and alloys.Dr. P C PandeyRoorkee Univ
Development of small gas turbine for jet belt.Dr. K L KumarIIT, Delhi
Mean drop size measuring technique in sprys using on optical system.Dr. K V L RaoNAL, Bangalore
Theoretical & experimantal investigation of certain problems in gas turbine.Dr. T K BoseIIT, Madras
Aerodynamics of mixed flow compressorDr. B C DuttaIISc, Bangalore
Studies on generation and suppression of the exhaust noise of turbojet engines.Dr. M L MunjalIISc, Bangalore
Evaluation of comparative performance of film cooling configuration for combustion chamber lines.Sh. B R PaiNAL, Bangalore
Development of hybrid propulsion system.Prof. V K JainIISc, Bangalore
Reacting turbulant flows in wakes and jets.Dr. R K SulleryIIT, Kanpur
Investigation of flow through vaned diffusers compressor.Dr. K L KumarIIT, Delhi
Development of a twin beam optical probe for measurement of velocity of turbulance in turbomachines.K ShivshankarNAL, Bangalore
Electrical control of propellant combustion.Dr. T P PandyaLucknow Univ
Investigation in vibration of transonic compressor rotor blades having low thickness and aspect ratio.Dr. S K SaneIIT, Bombay
Rapid response measurement techniques turbomachines.Sh. HariharanIISc, Bangalore
Rotating stall in axial impellers and secondary flow in compressor cascades.Dr. S SoudaranayagamIISc, Bangalore
Role of substituent groups and energetic atoms of fuel binders propellants combustion.Dr. H L GirdharKashmir Univ
Studies on premixed type combustor.Prof. ChittawadgiIIT, Bombay
Development of a reversible flow of combustion chamber.Prof. K N DamodaranIIT, Madras
Heat transfer in rotating balde and nozzles.Dr. A K MahantyIIT, Kharagpur
Annular boundary layers in axial compressors.Sh. VenkateshwaranIISc, Bangalore
Development of data acquisition system for flow investigation on a contra rotating axial flow compressor.Dr. P B SharmaIIT, Delhi
Development of theoretical and experimental models for simulation of squeeze filmed two spool rotors projects.Sh. Rahul BasuGTRE, Bangalore
Experimental study of turning supersonic cmpressor cascades.Prof. B C DuttaIISc, Bangalore
Hot cascade test rig.Prof. T K BoseIIT, Madras
Film cooling studies of turbine blade.Sh. V KrishnamurthyNAL, Bangalore
Aerodynamics and cooling performance investigation of massive multiple row discrete hole film cooled turbine blades.Sh. M D ManickamNAL, Bangalore
Model studies on combustion of composite.Prof. V K JainIISc, Bangalore B
Development of an axisymmetric supersonic air intake for ramjet.Dr. DamodaranIIT, Madras
Performance investigation of labyrinth seals.Sh. Nanjunda RaoGTRE, Bangalore
Studies towards establishing propulsion characteristics during flight of an airbreathing vehicle.Prof. S M DeshpandeIISc, Bangalore
Effect of fuel properties on gas turbine combustor performance.Sh MS ChidanandaNAL, Bangalore
Studies on fuel fed systems for a reversible type combustion chamber.Prof. DuttaIISc, Bangalore
Aerodynamic investigation of higher pressure ratio centrifugal impellers and their diffusers.Sh. ShankaranarayananNAL, Bangalore
Dynamics of pretwisted compressor rotor blades.Prof. S K SaneIIT, Bombay
Nozzle deposition problem for airbreathing composite engines.Prof. S S GokhaleIIT, Madras
Boundary layers and stall in turbo machines.Prof. S SoudaranayagamIISc, Bangalore
3 dimensional flow in arbitrary impellers.Prof. S SoudaranayagamIISc, Bangalore
Development of gas turbine fuel control system using microprocessor.Dr. K A DamodaranIIT, Madras
Application of software analysis of combustor turbo machinery.Dr. T R ShabarkarNAL, Bangalore
Mathematical modelling & development of a computer programme for the design of a gas turbine after burner system.Dr. V P SinghNaval College of Engg, Lonaval
Aeroengine blade and rotor dynamics.Dr. K GuptaIIT, Delhi
Surge and stall studies in an axial compressor.Dr. P B SharmaIIT, Delhi
Heat transfer studies pertaining to turbine blades.Dr. A K MahantyIIT, Kharagpur
Development of SFRJ for a gun launched projectile.Dr. K A DamodaranIIT, Madras
Experimental investigation of droplet burning behaviour in the presence of flame interference.Dr. A K GhoshIIT, Kharagpur
Self pyrolysable polymers as fuel rich propellant in air augmented missile.Prof. K KishoreIISc, Bangalore
Computation and experimental investigation of flame speeds in laminar and turbulent flow.Prof. H S MukundaIISc, Bangalore
Swirling flow in annuli with curved wells.Prof. S SoudaranayagamIISc, Bangalore
Study of tandane bladed compressor blade cascade.Dr. Bhaskar RoyIIT, Bombay
Implemntation of compressor computation programme.Prof. SoundaranayagamIISc, Bangalore
Some studies on solid propellant combustion.Prof. V K JainIISc, Bangalore
Multifunction nozzles.Sh. ChidanandaNAL, Bangalore
Prediction of flow with supercritical cascades using time marching techniques.Sh. A GirigoswamiNAL, Bangalore
Development of controlled diffusion airfoils (supercritical airfoils) for advanced axial flow compressors.Sh. K MohanNAL, Bangalore
Development of novel technique for cooling turbine blades.Dr. B R PaiNAL, Bangalore
Studies on energetic materilas.Dr. Gurdip SinghGorakhpur Univ
Investgative studies on foil bearing.Sh. S RamamurthyNAL, Bangalore
Aerodynamic and heat transfer studies of HPT rotor and stator blades of GTX-35VS engine.Dr. B R RaiNAL, Bangalore
The Rmokinetic and combustion studies of energetic composites.Dr. H L GirdharKashmir Univ
Design and analysis of flow through contra rotating fan/ compressor.Dr. Bhaskar RoyIIT, Bombay
Experimental investigation of heat transfer & flow through the internal cooling passage of cooled gas turbine.Dr. V KrishnamurthyNAL, Bangalore
Investigations in squeeze film damping of high speed rotor systems.Dr. R W ShewndeIIT, Bombay
Inlet distortion studies in compressors.Dr. N VenkatrayuluIIT, Madras
Studies on polyvinylnitrate as a high energy materialin rocket propellants.Sh. U G DurgapalIAT, Pune
3-D conduction code for temperature distribution using FEM for GT Blades.Prof. K N SeetharamuIIT, Madras
Studies on the mixing & combustion phenomenon in ramjet combustion chambers.Sh. R NatarajanIIT, Madras
Axial compressor stage performance improvements using end bend stators.Dr. P B SharmaIIT, Delhi
Investigation of swirling flow in vaned radial diffusers for high pressure centrifugal compressors.Dr. D P AggarwalIIT, Delhi
Numerical prediction of turbulent flow heat transfer in a gas turbine blade cooling passage with ribbed roughness.Sh. A W DateIIT, Bombay
Computer modelling of two stroke engines for RPV applications.Dr. V GanesanIIT, Madras
Experimental studies on aeroengine rotor dynamics transient and squeeze film damper effects.Dr. K GuptaIIT, Delhi
Expert system for rotor dynamics.Dr. R P ShimpiIIT, Bombay
Erosive burning studies of solid propellants under transonic and supersonic cross flow mach numbers.Dr. S KrishnanIIT, Madras
Design & rotor blades due to combined effects of vibratory and thermal loads.Prof. J S RaoIIT, Delhi
Ttransition in 3-D flows in turbo machines.Dr. S SoudaranayagamIISc, Bangalore
Numerical prediction of two dimensional reacting flows with application to ramjet combustion.Dr. R NatarajanIIT, Madras
Development of a computer code in curvilinear coordinates for small gas turbine components.Dr. D P AggarwalIIT, Delhi
Investigations of effect of cooling air injection on boundary layer and wake characteristics in case of the turbine.Sh. M D ManickamNAL, Bangalore
Studies on control of rotating stall in high speed axial flow compressors.Sh. Q H NagpurwalaNAL, Bangalore
Heat transfer in rotating coolant passages of gas turbine blades.Dr. V KrishnamoorthyNAL, Bangalore
Study of gas turbine combustion using air blast atomisers.Dr. S K SomIIT, Kharagpur
Computer aided instruction for air breathing propulsion.Dr. Gokhale & Prof. MukundaIIT, Madras
Tip clearance flows in compressors.Dr. N VenkatrajuluIIT, Madras
Heat transfer in rotating serpentine passages with and without rib turbulators.Dr. R P VedulaIIT, Bombay
Surface curvature effects on film cooling with and without imposed pressure gradient.Dr. R P VedulaIIT, Bombay
Feasibility study on the use of Wankal Engine for aeronautical applications.Sh. K SivasankaramNAL, Bangalore
Removal of aromatic hydrocarbons from light petroleum fraction by hydrogenation.Dr. S R PatwardhanIIT, Bombay
Studies in mixin process in low bypass turbofan engine.Dr. S D SharmaIIT, Bombay
Estimation of blade damping using finite element modelling.Prof. C V RamakrishnanIIT, Delhi
Software development for life estimation of turbine blades.Dr. J S Rao &
Prof. N S Vyas
IIT, Kanpur & IIT, Delhi
Dev of a 3-D eular code using time marching computational technique for propulsion fa applications.Sh. H GirigaswamiNAL, Bangalore
Design & dev of an early warning system of onset of compressor surge.Prof. S K SaneIIT, Bombay
3-D effects in diffusers.Prof. R C MalhotraIIT, Delhi
Feasibility studies for a small gas turbine engine development.Dr. K MurugesanNAL, Bangalore
Numerical tool for design of ejector supercharging of ground level bed test to simulate high mach entry.Prof. A G MaratheIIT, Bombay
Thermophoretic augmentation of aerosal particle transport in gas turbines (phase-I).Sh. K JayarajREC, Calicut
Tip clearance effects in an axial flow compressor stage.Prof. P B SharmaDCE, Delhi
Pyrolisable polymers as fuel rich propellants for Ram Rockets.Dr. S P PandaIAT, Pune
Effect of gust and freestream turbulance on flow past cascade.Dr. T K SenaguptaIIT, Kanpur
Development of noval techniques for cooling turbine blades phase II.R LakshminarayananNAL, Bangalore
Development of a flow solver for 2-D compressible flows in complex geometries and extended to 3-D flow.D P AgarwalIIT, Delhi
Computer & graphics based instruction for rocket propulsion.Dr. N K S RajanIISc, Bangalore
Design of multivariable controller for gas turbine engine.Sh. A SantharamNAL, Bangalore
Boundary layer and flow studies for design and development of highly loaded blade profiles for axial flow compressor.Dr. Bhaskar RoyIIT, Bombay
Investigations of a multiphase jet mixing and combustion in a dump combustor.Dr. R NatarajanIIT, Madras
Computational flow studies for development of highly loaded blade profiles for axial flow compressors.Dr. J C MandalIIT, Bombay
Wankel Engine Studies Phase II.Sh. K SivasankaranNAL, Bangalore
Influence of geometric nonlinearities, composite coupling effects.Dr. K B SubramanyamNBKR Institute
Demonstration of a small gas turbine based core engine.Dr. K MurgesanNAL, Bangalore
Dynamic modelling of compressor for stall and surge.Prof. S K SaneIIT, Bombay
Virtual Instrumentation for rotor dynamic applications.Dr. N S VyasIIT, Kanpur
Numerical prediction of flow and combustion in gas turbine combustion system.Dr. V GanesanIIT, Madras
Further erosive burning studies of solid propellants under transonic & supersonic cross flow mach numbers.Dr. S KrishananIIT, Madras
Investigations of aerodynamic & thermal performance of turbine blade trailing edge ejection.Dr. M D ManickamNAL, Bangalore
Study of radial combustor design.Dr. T R ShembharkarNAL, Bangalore
Prediction of shock boundary layer interaction in 3-D internal flow.Dr. K S RavichandranNAL, Bangalore
Investigations on supression of rotating stall in high speed axial flow compressors through boundary layer control.Q H NagpurwalaNAL, Bangalore
Heat transfer of pressure drop studies to identify configurations in rotating gas turbine coolant passage for improved.Dr. R P VedulaIIT, Bombay
Modelling of isothermal and reacting flows in afterburners.Prof. V GanesanIIT, Madras
Stall inception in centrifugal compressor.Dr. S RamamurthyNAL, Bangalore
Design & Development of speckle pattern interfrometric system for measurement monitoring of vibration.Dr. Chandra ShekherIIT, Delhi
CFD simulation of cold and reacting flows in reverse flow gas turbine combustor.Prof. S N GuptaIIT, Delhi
Linear and Non-linear parameter estimation in rotor bearing systems.Dr. NS VyasIIT, Kanpur
Non linear dynamics and control of surge oscillations in axial flow compressorsDr. Sanjay P BhatIIT, Bombay
Studies on supersonic mixing and combustion.Dr. Job KurianIIT, Madras
Assessment of L/D ratio for virtual and artificial birds and characterisation of birds flow on engine components.Dr. K RamchandraGTRE, Bangalore
Non linear dynamics and control of surge oscillations in axial flow compressors.Dr. Sanjay P BhatIIT, Bombay
A three dimensional Navier Strokes analysis for a film cooled rotating blade.Dr. Subrata SarkarIIT, Kanpur
Investigative studies on elastomer dampers for rotating systems.Dr. V Arun KumarNAL, Bangalore
Study of hot jet aeroacoustics.Prof. T S SheshadriIISc, Bangalore
Numerical prediction of flows through swirlers.Prof. V GanesanIIT, Madras
Computer aided analysis and design of high speed ball and roller bearings.Dr. R TiwariIIT, Guwahati
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