SlideShare a Scribd company logo
1 of 3
Arundhathi G. Krishnan 
“SOWPARNIKAA” 102/2,12th main Road, Maruthi Nagar, Malleshpalaya Main Road, Bangalore- 560075 
 25342277 (Res) , M 9880933900 Email : nidhi64@hotmail.com 
An experienced IT professional with a significant experience in Aerospace Design Engineering. Looking to 
contribute in a technically challenging project environment for the growth of organization and self. 
Summary of Experience 
· A proven leader with excellent interpersonal skills including strong decision making, communications 
and effective interactions with colleagues, technical solution delivery experts, and senior leaders. 
· 20 years of domain experience in Centre for Civil Aircraft Design and Development(C-CADD), a division 
of National Aerospace Lab, Bangalore . 
· Worked with Aerodynamics group to assist them in wind tunnel data analysis, to calculate 
aerodynamic loads, to generate performance and graphical representation of aircraft parameters 
· Presented a paper on interactive data base management system for quick retrieval and analysis of wind 
Tunnel test data in a conference at Indian Institute of Science, Bangalore. 
· Skilled in the use of Microsoft Word, Excel and PowerPoint. 
· Published many technical papers in NAL, Bangalore 
Computer Languages known : C, SDK, FORTRAN, X-WINDOWS, BASIC 
Packages known : GKS, INGRES 6.4, dBASE III 
Operating Systems known : AIX, UNIX, DOS, MS-WINDOWS 
Program Experiences 
1. Aerospace Design Engineers Pvt. Ltd., NAL, Bangalore : (August 1995 - April 2014 ) 
· The Hybrid Vortex Lattice Method (HVLM) program developed in-house is widely used for calculation of 
aerodynamic forces and moments on arbitrary aircraft configuration at C-CADD. This program has been 
extensively executed for the generation of aerodynamic data including panel loads for SARAS and 
HANSA 
· Developed Graphical User Interface for pre & post processing of data for the above package using 
Graphic Kernel System (GKS with FORTRAN binding). Following are special features included in the 
package. 
· On-Line Help 
· Built-in error checks for wrong entries 
· Optional on-line viewing of geometry during input data entry 
· Viewing of panel plot 
· On-Line plotting of Output Aerodynamic Quantities including span wise Load Distribution on 
Wing, HT etc.
· Cp Distribution on Fuselage & Nacelle at various azimuthal angles and plots of Cross 
Sectional Cps at given body station 
· Involved in the development of interactive user friendly software package for estimating aerodynamic 
loads for SARAS PT1 and PT2 using HVLM without altering the master data. Also developed a package 
to store and retrieve the useful outputs generated by HVLM for SARAS and HANSA. 
· Participated in computing ice shapes for SARAS lifting surfaces using an interactive computer program 
‘SARASICE’, developed in house using 2-d ONERA code. Ice shapes can be predicted for any given input 
data and atmospheric conditions using this program 
· Developed a user friendly and interactive data base management system for quick retrieval and 
analysis of Wind Tunnel test data generated on SARAS aircraft scaled models. 
Main features of the package: 
· Useful in quick retrieval of data 
· Comparison and plotting of data from various tunnels, versions, flow conditions and 
configurations 
· Graph reading, calculation of slope and maxima / minima. 
· Support for screen dump / color post-script printout. 
· Updating database as well as the program to accommodate the new data types (for example Cp 
distributions, power model test results) 
· Involved in computing performance quantities for SARAS PT1 and PT2. Performance parameters 
included take-off and landing distances, cruise 
· Performance and point performance quantities like max speed, specific range, rate of climb etc. Engine 
parameters for PT66 and PT67 using Hartzell and MT propeller charts respectively were estimated as 
and when required using EEPP package supplied by the engine manufacturer. 
· Development of 2-D and 3-D plotting package on UNIX platform. Developed on IBM RS/6000 system 
under AIX 4.1.5 Operating System 
Graphical platform used – GKS with FORTRAN binding on X-terminal, 
HFT or emulated X window. 
· 2-D plotting package can do data analysis like derivative estimation, cross plot, correlation plot etc. and 
drive postscript devices. 
· Developed extensive postscript routines for production of report quality hardcopy outputs on 
postscript devices. 
· 3-D plotting depicts arbitrary paneled aircraft geometry in orthographic views. It can do local zooming 
and panning. Hidden line removal achieved using normal projection algorithm and painter’s algorithm. 
· Involved in software development for analysis of various data using Wavelet Transform Techniques. 
This involved using windows (3.1) SDK under ‘C’ for trouble shooting and bug fixing of packages 
developed in the group. 
PUBLICATIONS: 
· Database management system for SARAS wind tunnel test data, PDCA0010, April 2000, Arundhathi G. 
Krishnan, Rajeswari S Ramamurthy, Malini Parthasarathy 
· User’s manual for the analysis of aircraft configurations using hybrid vortex lattice method (HVLM), 
PDCA 0101, January 2001, Arundhathi G. Krishnan, Rajeswari S Ramamurthy
· Improvements made in DBMS package for SARAS wind tunnel data to include fuselage Cp 
measurements and hinge moments, PDCA0301, May 2003, Arundhathi G. Krishnan, Shanthala 
Shivakumar, Rajeswari S Ramamurthy 
· Ice shapes on SARAS wing, HT and VT using the ONERA 2-d icing code PDCA0502, December 2005, 
Rajeswari S Ramamurthy, Arundhathi G. Krishnan 
· Interactive user friendly software package for estimating aerodynamic loads for SARAS PT1 and PT2 
using HVLM, PDCA0604, December 2006, Arundhathi G. Krishnan, Rajeswari S Ramamurthy 
· Modifications in the Wind Tunnel Data Base Management package to include Rudder Hinge Moment 
data of Saras, PDCA1007, October 2010, Arundhathi G. Krishnan 
· Power, Fuel flow & Thrust Data report for Saras, Arundhathi G. Krishnan, G.K. Panda, 
SARAS/AERO/2013, May 2013 
2. ISS, National Aerospace Laboratories, Bangalore (August 1994-July 1995) 
· Developed a software on INGRES 6.4 for a conference using 4GL coding in UNIX environment. Involved 
in the design, coding and testing of the above software. 
3. Ambience Engineering Pvt. Ltd., Bangalore: (July 1991-March 1993) 
Post: Customer Support Engineer 
· Testing, Maintenance and up gradation of computers and its accessories. 
· Quality Control & Pre-Installation Check tests at Regional Repair Centre 
· Worked as a Call coordinator in Planning Department. Conducted a Hardware Training Course. 
4. Transmatic Systems Ltd., Trivandrum (July 1987-January 1990) Post: Production Engineer 
· Testing and Trouble shooting of Microprocessor based Communication Systems like Electronic Telex 
Terminals, MODEM etc. Testing of various cards of on universal testing boards before assembly. 
· Supervision of PCB assembling, Wave soldering and other related production activities 
Education: 
University of Kerala - B.Tech in Electrical Engineering 74.7 % (First Class) College of Engineering, Trivandrum 
Vocational post-project training: Two months at VSSC, Thumba, Trivandrum 
Other qualification: Completed a six months course at M/s. Apple Industries Ltd., Bangalore covering UNIX, ‘C’ 
and Introduction to RDBMS. Project carried out during this course - ISAM functions under DOS

More Related Content

What's hot

IRJET- Accuracy Configurable Adder
IRJET- Accuracy Configurable AdderIRJET- Accuracy Configurable Adder
IRJET- Accuracy Configurable AdderIRJET Journal
 
Design and Implementation of Low-Power and Area-Efficient 64 bit CSLA using VHDL
Design and Implementation of Low-Power and Area-Efficient 64 bit CSLA using VHDLDesign and Implementation of Low-Power and Area-Efficient 64 bit CSLA using VHDL
Design and Implementation of Low-Power and Area-Efficient 64 bit CSLA using VHDLIJSRD
 
A Parallel Computing Model for Segmentation of Vehicle Number Plate through W...
A Parallel Computing Model for Segmentation of Vehicle Number Plate through W...A Parallel Computing Model for Segmentation of Vehicle Number Plate through W...
A Parallel Computing Model for Segmentation of Vehicle Number Plate through W...theijes
 
Implementation of Low Power and Area Efficient Carry Select Adder
Implementation of Low Power and Area Efficient Carry Select AdderImplementation of Low Power and Area Efficient Carry Select Adder
Implementation of Low Power and Area Efficient Carry Select Adderinventionjournals
 
Design and Verification of Area Efficient Carry Select Adder
Design and Verification of Area Efficient Carry Select AdderDesign and Verification of Area Efficient Carry Select Adder
Design and Verification of Area Efficient Carry Select Adderijsrd.com
 
Supporting Flight Test And Flight Matching
Supporting Flight Test And Flight MatchingSupporting Flight Test And Flight Matching
Supporting Flight Test And Flight Matchingj2aircraft
 
DESIGN AND PERFORMANCE ANALYSIS OF BINARY ADDERS_edited
DESIGN AND PERFORMANCE ANALYSIS OF BINARY ADDERS_editedDESIGN AND PERFORMANCE ANALYSIS OF BINARY ADDERS_edited
DESIGN AND PERFORMANCE ANALYSIS OF BINARY ADDERS_editedShital Badaik
 
IRJET - A Speculative Approximate Adder for Error Recovery Unit
IRJET - A Speculative Approximate Adder for Error Recovery UnitIRJET - A Speculative Approximate Adder for Error Recovery Unit
IRJET - A Speculative Approximate Adder for Error Recovery UnitIRJET Journal
 
Low power & area efficient carry select adder
Low power & area efficient carry select adderLow power & area efficient carry select adder
Low power & area efficient carry select adderSai Vara Prasad P
 
IRJET- A Review of Approximate Adders for Energy-Efficient Digital Signal Pro...
IRJET- A Review of Approximate Adders for Energy-Efficient Digital Signal Pro...IRJET- A Review of Approximate Adders for Energy-Efficient Digital Signal Pro...
IRJET- A Review of Approximate Adders for Energy-Efficient Digital Signal Pro...IRJET Journal
 
SB_MSC-Apex_Structures_LTR_pt
SB_MSC-Apex_Structures_LTR_ptSB_MSC-Apex_Structures_LTR_pt
SB_MSC-Apex_Structures_LTR_ptanandakumara MB
 
Gis saaf-project
Gis saaf-projectGis saaf-project
Gis saaf-projectSalah Bakry
 
Comparative Analysis of Various Grid Based Scheduling Algorithms
Comparative Analysis of Various Grid Based Scheduling AlgorithmsComparative Analysis of Various Grid Based Scheduling Algorithms
Comparative Analysis of Various Grid Based Scheduling Algorithmsiosrjce
 

What's hot (19)

IRJET- Accuracy Configurable Adder
IRJET- Accuracy Configurable AdderIRJET- Accuracy Configurable Adder
IRJET- Accuracy Configurable Adder
 
Data mining
Data miningData mining
Data mining
 
Design and Implementation of Low-Power and Area-Efficient 64 bit CSLA using VHDL
Design and Implementation of Low-Power and Area-Efficient 64 bit CSLA using VHDLDesign and Implementation of Low-Power and Area-Efficient 64 bit CSLA using VHDL
Design and Implementation of Low-Power and Area-Efficient 64 bit CSLA using VHDL
 
A Parallel Computing Model for Segmentation of Vehicle Number Plate through W...
A Parallel Computing Model for Segmentation of Vehicle Number Plate through W...A Parallel Computing Model for Segmentation of Vehicle Number Plate through W...
A Parallel Computing Model for Segmentation of Vehicle Number Plate through W...
 
Implementation of Low Power and Area Efficient Carry Select Adder
Implementation of Low Power and Area Efficient Carry Select AdderImplementation of Low Power and Area Efficient Carry Select Adder
Implementation of Low Power and Area Efficient Carry Select Adder
 
Design and Verification of Area Efficient Carry Select Adder
Design and Verification of Area Efficient Carry Select AdderDesign and Verification of Area Efficient Carry Select Adder
Design and Verification of Area Efficient Carry Select Adder
 
Supporting Flight Test And Flight Matching
Supporting Flight Test And Flight MatchingSupporting Flight Test And Flight Matching
Supporting Flight Test And Flight Matching
 
4. graphics standard
4. graphics standard4. graphics standard
4. graphics standard
 
DESIGN AND PERFORMANCE ANALYSIS OF BINARY ADDERS_edited
DESIGN AND PERFORMANCE ANALYSIS OF BINARY ADDERS_editedDESIGN AND PERFORMANCE ANALYSIS OF BINARY ADDERS_edited
DESIGN AND PERFORMANCE ANALYSIS OF BINARY ADDERS_edited
 
IRJET - A Speculative Approximate Adder for Error Recovery Unit
IRJET - A Speculative Approximate Adder for Error Recovery UnitIRJET - A Speculative Approximate Adder for Error Recovery Unit
IRJET - A Speculative Approximate Adder for Error Recovery Unit
 
Cathode ray tube
Cathode ray tubeCathode ray tube
Cathode ray tube
 
Low power & area efficient carry select adder
Low power & area efficient carry select adderLow power & area efficient carry select adder
Low power & area efficient carry select adder
 
IRJET- A Review of Approximate Adders for Energy-Efficient Digital Signal Pro...
IRJET- A Review of Approximate Adders for Energy-Efficient Digital Signal Pro...IRJET- A Review of Approximate Adders for Energy-Efficient Digital Signal Pro...
IRJET- A Review of Approximate Adders for Energy-Efficient Digital Signal Pro...
 
Numerical Control
Numerical Control Numerical Control
Numerical Control
 
ICFD12-EG-5044_final
ICFD12-EG-5044_finalICFD12-EG-5044_final
ICFD12-EG-5044_final
 
SB_MSC-Apex_Structures_LTR_pt
SB_MSC-Apex_Structures_LTR_ptSB_MSC-Apex_Structures_LTR_pt
SB_MSC-Apex_Structures_LTR_pt
 
Gis saaf-project
Gis saaf-projectGis saaf-project
Gis saaf-project
 
Comparative Analysis of Various Grid Based Scheduling Algorithms
Comparative Analysis of Various Grid Based Scheduling AlgorithmsComparative Analysis of Various Grid Based Scheduling Algorithms
Comparative Analysis of Various Grid Based Scheduling Algorithms
 
resume_Archi
resume_Archiresume_Archi
resume_Archi
 

Similar to Uma Sagar_c

Manuel_Olivares_Resume_LinkedIn_2016
Manuel_Olivares_Resume_LinkedIn_2016Manuel_Olivares_Resume_LinkedIn_2016
Manuel_Olivares_Resume_LinkedIn_2016Manuel Olivares
 
Larsen,dustin eng resume_june2016 - copy
Larsen,dustin eng resume_june2016 - copyLarsen,dustin eng resume_june2016 - copy
Larsen,dustin eng resume_june2016 - copyDustin Larsen
 
Artificial Intelligence Based Method for Obtaining Aerodynamic Characteristic...
Artificial Intelligence Based Method for Obtaining Aerodynamic Characteristic...Artificial Intelligence Based Method for Obtaining Aerodynamic Characteristic...
Artificial Intelligence Based Method for Obtaining Aerodynamic Characteristic...IRJET Journal
 
Maheswara reddy 10+years_avionics
Maheswara reddy 10+years_avionicsMaheswara reddy 10+years_avionics
Maheswara reddy 10+years_avionicsmaheswarareddy pr
 
Hard landing predection
Hard landing predectionHard landing predection
Hard landing predectionRAJUPADHYAY44
 
DOC245-20240219-WA0000_240219_090212.pdf
DOC245-20240219-WA0000_240219_090212.pdfDOC245-20240219-WA0000_240219_090212.pdf
DOC245-20240219-WA0000_240219_090212.pdfShaizaanKhan
 
A statistical approach to predict flight delay
A statistical approach to predict flight delayA statistical approach to predict flight delay
A statistical approach to predict flight delayiDTechTechnologies
 
Resume-Electronics Design Engineer
Resume-Electronics Design EngineerResume-Electronics Design Engineer
Resume-Electronics Design EngineerSachin N.P
 
Ali Fuat Berker _Resume_Sep 2016
Ali Fuat Berker _Resume_Sep 2016Ali Fuat Berker _Resume_Sep 2016
Ali Fuat Berker _Resume_Sep 2016Ali Fuat BERKER
 
Computer Aided Process Planning Using Neutral File Step for Rotational Parts
Computer Aided Process Planning Using Neutral File Step for Rotational PartsComputer Aided Process Planning Using Neutral File Step for Rotational Parts
Computer Aided Process Planning Using Neutral File Step for Rotational PartsRSIS International
 

Similar to Uma Sagar_c (20)

ct-acd32093-2
ct-acd32093-2ct-acd32093-2
ct-acd32093-2
 
Manuel_Olivares_Resume_LinkedIn_2016
Manuel_Olivares_Resume_LinkedIn_2016Manuel_Olivares_Resume_LinkedIn_2016
Manuel_Olivares_Resume_LinkedIn_2016
 
Resume
ResumeResume
Resume
 
Anderson_CV_NN
Anderson_CV_NNAnderson_CV_NN
Anderson_CV_NN
 
Larsen,dustin eng resume_june2016 - copy
Larsen,dustin eng resume_june2016 - copyLarsen,dustin eng resume_june2016 - copy
Larsen,dustin eng resume_june2016 - copy
 
chris guidice RESUME Ver2
chris guidice RESUME Ver2chris guidice RESUME Ver2
chris guidice RESUME Ver2
 
Artificial Intelligence Based Method for Obtaining Aerodynamic Characteristic...
Artificial Intelligence Based Method for Obtaining Aerodynamic Characteristic...Artificial Intelligence Based Method for Obtaining Aerodynamic Characteristic...
Artificial Intelligence Based Method for Obtaining Aerodynamic Characteristic...
 
USA Valid H1b-Structural Engineer-SuryaM
USA Valid H1b-Structural Engineer-SuryaMUSA Valid H1b-Structural Engineer-SuryaM
USA Valid H1b-Structural Engineer-SuryaM
 
Resume_neeraj
Resume_neerajResume_neeraj
Resume_neeraj
 
Maheswara reddy 10+years_avionics
Maheswara reddy 10+years_avionicsMaheswara reddy 10+years_avionics
Maheswara reddy 10+years_avionics
 
Prem Resume with Ref
Prem Resume with RefPrem Resume with Ref
Prem Resume with Ref
 
Dhananjay_Mishra
Dhananjay_MishraDhananjay_Mishra
Dhananjay_Mishra
 
Clusetrreport
ClusetrreportClusetrreport
Clusetrreport
 
Hard landing predection
Hard landing predectionHard landing predection
Hard landing predection
 
DOC245-20240219-WA0000_240219_090212.pdf
DOC245-20240219-WA0000_240219_090212.pdfDOC245-20240219-WA0000_240219_090212.pdf
DOC245-20240219-WA0000_240219_090212.pdf
 
A statistical approach to predict flight delay
A statistical approach to predict flight delayA statistical approach to predict flight delay
A statistical approach to predict flight delay
 
Fu3310321039
Fu3310321039Fu3310321039
Fu3310321039
 
Resume-Electronics Design Engineer
Resume-Electronics Design EngineerResume-Electronics Design Engineer
Resume-Electronics Design Engineer
 
Ali Fuat Berker _Resume_Sep 2016
Ali Fuat Berker _Resume_Sep 2016Ali Fuat Berker _Resume_Sep 2016
Ali Fuat Berker _Resume_Sep 2016
 
Computer Aided Process Planning Using Neutral File Step for Rotational Parts
Computer Aided Process Planning Using Neutral File Step for Rotational PartsComputer Aided Process Planning Using Neutral File Step for Rotational Parts
Computer Aided Process Planning Using Neutral File Step for Rotational Parts
 

Uma Sagar_c

  • 1. Arundhathi G. Krishnan “SOWPARNIKAA” 102/2,12th main Road, Maruthi Nagar, Malleshpalaya Main Road, Bangalore- 560075  25342277 (Res) , M 9880933900 Email : nidhi64@hotmail.com An experienced IT professional with a significant experience in Aerospace Design Engineering. Looking to contribute in a technically challenging project environment for the growth of organization and self. Summary of Experience · A proven leader with excellent interpersonal skills including strong decision making, communications and effective interactions with colleagues, technical solution delivery experts, and senior leaders. · 20 years of domain experience in Centre for Civil Aircraft Design and Development(C-CADD), a division of National Aerospace Lab, Bangalore . · Worked with Aerodynamics group to assist them in wind tunnel data analysis, to calculate aerodynamic loads, to generate performance and graphical representation of aircraft parameters · Presented a paper on interactive data base management system for quick retrieval and analysis of wind Tunnel test data in a conference at Indian Institute of Science, Bangalore. · Skilled in the use of Microsoft Word, Excel and PowerPoint. · Published many technical papers in NAL, Bangalore Computer Languages known : C, SDK, FORTRAN, X-WINDOWS, BASIC Packages known : GKS, INGRES 6.4, dBASE III Operating Systems known : AIX, UNIX, DOS, MS-WINDOWS Program Experiences 1. Aerospace Design Engineers Pvt. Ltd., NAL, Bangalore : (August 1995 - April 2014 ) · The Hybrid Vortex Lattice Method (HVLM) program developed in-house is widely used for calculation of aerodynamic forces and moments on arbitrary aircraft configuration at C-CADD. This program has been extensively executed for the generation of aerodynamic data including panel loads for SARAS and HANSA · Developed Graphical User Interface for pre & post processing of data for the above package using Graphic Kernel System (GKS with FORTRAN binding). Following are special features included in the package. · On-Line Help · Built-in error checks for wrong entries · Optional on-line viewing of geometry during input data entry · Viewing of panel plot · On-Line plotting of Output Aerodynamic Quantities including span wise Load Distribution on Wing, HT etc.
  • 2. · Cp Distribution on Fuselage & Nacelle at various azimuthal angles and plots of Cross Sectional Cps at given body station · Involved in the development of interactive user friendly software package for estimating aerodynamic loads for SARAS PT1 and PT2 using HVLM without altering the master data. Also developed a package to store and retrieve the useful outputs generated by HVLM for SARAS and HANSA. · Participated in computing ice shapes for SARAS lifting surfaces using an interactive computer program ‘SARASICE’, developed in house using 2-d ONERA code. Ice shapes can be predicted for any given input data and atmospheric conditions using this program · Developed a user friendly and interactive data base management system for quick retrieval and analysis of Wind Tunnel test data generated on SARAS aircraft scaled models. Main features of the package: · Useful in quick retrieval of data · Comparison and plotting of data from various tunnels, versions, flow conditions and configurations · Graph reading, calculation of slope and maxima / minima. · Support for screen dump / color post-script printout. · Updating database as well as the program to accommodate the new data types (for example Cp distributions, power model test results) · Involved in computing performance quantities for SARAS PT1 and PT2. Performance parameters included take-off and landing distances, cruise · Performance and point performance quantities like max speed, specific range, rate of climb etc. Engine parameters for PT66 and PT67 using Hartzell and MT propeller charts respectively were estimated as and when required using EEPP package supplied by the engine manufacturer. · Development of 2-D and 3-D plotting package on UNIX platform. Developed on IBM RS/6000 system under AIX 4.1.5 Operating System Graphical platform used – GKS with FORTRAN binding on X-terminal, HFT or emulated X window. · 2-D plotting package can do data analysis like derivative estimation, cross plot, correlation plot etc. and drive postscript devices. · Developed extensive postscript routines for production of report quality hardcopy outputs on postscript devices. · 3-D plotting depicts arbitrary paneled aircraft geometry in orthographic views. It can do local zooming and panning. Hidden line removal achieved using normal projection algorithm and painter’s algorithm. · Involved in software development for analysis of various data using Wavelet Transform Techniques. This involved using windows (3.1) SDK under ‘C’ for trouble shooting and bug fixing of packages developed in the group. PUBLICATIONS: · Database management system for SARAS wind tunnel test data, PDCA0010, April 2000, Arundhathi G. Krishnan, Rajeswari S Ramamurthy, Malini Parthasarathy · User’s manual for the analysis of aircraft configurations using hybrid vortex lattice method (HVLM), PDCA 0101, January 2001, Arundhathi G. Krishnan, Rajeswari S Ramamurthy
  • 3. · Improvements made in DBMS package for SARAS wind tunnel data to include fuselage Cp measurements and hinge moments, PDCA0301, May 2003, Arundhathi G. Krishnan, Shanthala Shivakumar, Rajeswari S Ramamurthy · Ice shapes on SARAS wing, HT and VT using the ONERA 2-d icing code PDCA0502, December 2005, Rajeswari S Ramamurthy, Arundhathi G. Krishnan · Interactive user friendly software package for estimating aerodynamic loads for SARAS PT1 and PT2 using HVLM, PDCA0604, December 2006, Arundhathi G. Krishnan, Rajeswari S Ramamurthy · Modifications in the Wind Tunnel Data Base Management package to include Rudder Hinge Moment data of Saras, PDCA1007, October 2010, Arundhathi G. Krishnan · Power, Fuel flow & Thrust Data report for Saras, Arundhathi G. Krishnan, G.K. Panda, SARAS/AERO/2013, May 2013 2. ISS, National Aerospace Laboratories, Bangalore (August 1994-July 1995) · Developed a software on INGRES 6.4 for a conference using 4GL coding in UNIX environment. Involved in the design, coding and testing of the above software. 3. Ambience Engineering Pvt. Ltd., Bangalore: (July 1991-March 1993) Post: Customer Support Engineer · Testing, Maintenance and up gradation of computers and its accessories. · Quality Control & Pre-Installation Check tests at Regional Repair Centre · Worked as a Call coordinator in Planning Department. Conducted a Hardware Training Course. 4. Transmatic Systems Ltd., Trivandrum (July 1987-January 1990) Post: Production Engineer · Testing and Trouble shooting of Microprocessor based Communication Systems like Electronic Telex Terminals, MODEM etc. Testing of various cards of on universal testing boards before assembly. · Supervision of PCB assembling, Wave soldering and other related production activities Education: University of Kerala - B.Tech in Electrical Engineering 74.7 % (First Class) College of Engineering, Trivandrum Vocational post-project training: Two months at VSSC, Thumba, Trivandrum Other qualification: Completed a six months course at M/s. Apple Industries Ltd., Bangalore covering UNIX, ‘C’ and Introduction to RDBMS. Project carried out during this course - ISAM functions under DOS