tool design i, catia v5

CURRICULAM VITAE

G. PANDIKUMAR

FBM ***, HAL Township

Marathahalli Post

Banagalore-560 037 Mobile No. : 903-***-****

E-mail: *************@*****.***

EXPERIENCE SUMMARY:

I am working as Manager in Hindustan Aeronautical Ltd, leading the Aerospace Industry under Ministry of Defence – Govt. of India geared for Design, Development, Manufacturing and overhauling of Aerospace Vehicles. I have excellent knowledge on Tool Design using CATIA V5, Checking and release of Tool Drawing. And also have good knowledge on Design and Analysis and worked on various analysis projects in Flight test, wind tunnel test and computation of Maneuvering Loads.

PROFESSIONAL QUALIFICATIONS:

M. Tech in Aerospace Engineering from Indian Institute of Technology, Kanpur, during 1997 with 76.70%

B. Tech In Aeronautical Engineering from Madras Institute of Technology, Anna University, Chennai, during 1995 with 65.50%

B. Sc in Mathematics from Madurai Kamarajar University, during 1992 with 73.70%

WORK EXPERIENCE : Total 13+ Years

From July 2008 to till date : Working as a Manager (Tool Design) at Composite

Manufacturing Division, Hindustan

Aeronautics Limited, Bangalore.

From July 2005 to June 2008 : Working as a Deputy Manager (Design) at Aircraft

Research and Design Center, Hindustan

Aeronautics Limited, Bangalore.

From June 2001 to June 2005 : Worked as a Design Engineer at Aircraft

Research and Design Center, Hindustan

Aeronautics Limited, Bangalore.

From Dec 1999 to June2001 : Worked as a Assistant Engineer at Aircraft Division

Hindustan Aeronautics Limited, Bangalore.

From Dec 1998 to Nov 1999 : Worked as a Project Engineer at Aircraft Division

Hindustan Aeronautics Limited, Bangalore.

From July 1998 to Nov 1998 : Worked as Post graduate Trainee at National

Aerospace Laboratory. Bangalore.

SKILL SETS:

Feature based Parametric Solid and Surface Modeling, Assembly Modeling and Manufacturing Drawings using CATIA V5

Experimental and Theoretical Aerodynamics

Gas dynamics and Propulsion

Performance of Aircraft

Flight test analysis of Aircraft

COMPUTER PROFICIENCY:

Operating System : Windows, NT, XP

Language : Fortran

Packages : MS Office

Technical Software : CATIA V5

Technical Projects Profile:

Project 1 : Designing of ALH Tools using CATIA V5

Organisation : HAL, Bangalore

Description : Plan, Design, Modeling and Drafting Master model, Composite and Metallic Layup tool. And Assembly tool, Trimming fixture, Machining fixture etc., Checking and release of tool design for manufacture

Project 2 : Variation of Climb Performance from the flight test data

Organisation : HAL, Bangalore

Description : Flight data was scanned to identify the steady climb segments in these flights. A math model was formulated and results from the math model are compared against flight test results, allowing for known parameter variations in flight. There is a good agreement between the two. The comparison of time to climb from math model and Flight data shows that the comparison is good.

Project 3 : Result of High Speed Wind Tunnel test with External Stores.

Organisation : HAL, Bangalore

Description : High speed wind tunnel tests were carried out to establish the symmetric effects of wing mounted and fuselage mounted external stores. The tests were carried out to provide variation of aerodynamics characteristic with angle of attack, sideslip and Mach number. Control effectiveness with stores was also evaluated.

Project 4 : Theoretical computation of Maneuvering Loads of Aircraft

Organisation : HAL, Bangalore

Description : Theoretical analysis of maneuvering Loads with Variation of Mach No., Load factor, angle of attack and sideslip angle for Aerospace Vehicle.

ACHIVEMENTS:

Qualified in GATE-1996 for under gone M.Tech studies at IIT, Kanpur through

Government of India Scholarship.

Professional AFFILIATION:

Life Member of the Aeronautical Society of India, Newdelhi

ACADEMIC projecTs:

Degree : M. Tech

Title : Studies on the effect 0f initial conditions on the mixing and noise characteristics of a supersonic free jet.

Institute : Indian Institute of Technology, Kanpur

Description : The effect of nozzle divergence angle and nozzle length on the jet propagation and noise has been investigated experimentally. Free jets issuing from convergent-divergent axisymmetric nozzles at Mach 2 have been studied. Jets from 4 nozzles of different divergent angle have been investigated. One nozzle with q =3o, length 14.30 mm and exit diameter 6.50 mm was kept as the basic no0zzle. In addition to these geometrical parameters, the stagnation pressure was also varied from 3 atm to 6 atm. The jet decay was analyzed by measuring the centerline Pitot pressure. The pressure profiles across the jet at different axial locations were also measured. The shock cell length in the jet core was measured directly. The shock pattern in the core was visualized with shadowgraph technique.

The jet noise was measured at two orientations by measuring the overall sound pressure level. The noise directly at the nozzle exit was also measured.

PERSONAL PROFILE:

Father’s Name : K. GOPAL.

Date Of Birth : 30-12-1969

Passport No. : U-037565

Marital status : Married

Current CTC : 12 lac/year

Expected CTC : 18 lac/Year in India

Notice Period : 3 Months

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