Coresoft Inc Delhi/NCR : CAD Engineer

[mskavi]

Coresoft Inc.
http://www.caddcentre.ws

Keywords: AutoCAD, CAD, Revit, Photoshop, Interior Designer, Architect, Draughtman, Design, ArchiCAD, 3ds Max, Maya, Project Management, Primavera, MS Project, Engineering Design

Designation: CAD Engineer
Experience: 1 - 4 Years
Location: Delhi/NCR
Compensation:
As per Industry Norms, Good Incentives.
Education: UG - Any Graduate - Any Specialization
PG - Post Graduation Not Required
Industry Type: Education/ Teaching/Training
Functional Area: Architecture, Interior Design
Posted Date: 07 Jan 2009

Job Description
* To organise and conduct the courses.
* Responsible for providing training on softwares like... AutoCAD, 3ds Max, ArchiCAD, Revit, Maya, Flash, Photoshop, MSP, Primavera.
* Responsible for handling corporate batches.
* Good Learning Environment.
* Advanced level training will be given to the candidates.

Desired Candidate Profile
* Degree holder from a reputed institute.
* Good communication skills.
* Can handle corporates.
* Good learner.
* Knowledge of AutoCAD is must.

Company Profile
CADD Centre is a 19 year old company and has the largest training centre networks in the world. Our courses on CAD, PPM and Grafx are widely accepted and our instructional excellence is well regarded.Our courses are industry specific.

Read Coresoft Inc. Blog

Executive Name: Ms. Soni Pandey

Address:
Coresoft Inc
S.C.O 21, 2nd floor,
Old Delhi Road,
Sector - 14,
Gurgaon,Harayana,INDIA 122001

Email Address: cadd_gurgaon@rediffmail.com

Telephone: 91-124-4103105

Reference ID:
Jan-09/IAD

[Guest-IJT]

Name : RAJA. M. DALAL
Email : rajadalal32 AT gmail.com
Designation / Skillset : Trainee/junior cad Engineer
B.E Mechanical Fresher

Resume :

CAREER OBJECTIVE :
Looking for an opportunity to explore my capabilities in a modern work environment with a growth potential a challenging position, utilizing my abilities developed through my education, with the opportunity for professional growth based on performance.
EDUCATIONAL CREDENTIALS :
COURSE YEAR OF PASSING UNIVERSITY MARKS IN PERCENTAGE
S.S.L.C 2004-05 Aurangabad 71.46
12th 2006-07 Aurangabad 64.67
B.E(Mechanical) 2011 V.T.U, Belgaum 72.3
STRENGTHS :

Positive attitude, Active Participation, smart working nature
Sincere and Punctual
Ability to work any place
FINAL YEAR PROJECT :
TITLE :
Stress Analysis of a Transport Aircraft Wing Bottom Skin Panel With Landing Gear Cutout in
Bangalore Aircraft Industries [BAIL] INDIA PVT LTD.
ABOUT THE PROJECT :
Objective :
The objective of this project is to ensure the structural safety of the aircraft wing from static and fatigue loading point of view through analytical approach by carrying out stress analysis and calculation of fatigue life to crack initiation.
Abstract :
This project addresses the issue of identification of highest tensile stress location in a typical wing of Transport aircraft. To start with this requires the stress analysis of a wing under critical load distribution that the airframe is going to be subjected to. This identifies the location of high tensile stress which is the potential location for fatigue crack initiation.
For this project we select the location in the wing where there is a stress concentration. A panel consisting of integral stiffeners and landing gear cutout is considered. Few- iterations are carried out to accurately predict the highest tensile stress location.
Prediction of life to fatigue crack initiation from the highest tensile stress location will be carried out.
Brief description :
Airplanes require landing gear for taxiing, takeoff, and landing. To accommodate the landing gear a cutout is provided in the aircraft wing. These cut outs will introduce stress concentration regions in the wing. The stress concentration regions are the probable locations for fatigue crack initiation. The identification of such fatigue crack initiation locations and carrying out the calculation of fatigue life to crack initiation is important to ensure the safety of the structure. This project work is focused on stress analysis of a panel consisting of landing gear cut out and calculation of fatigue life to crack initiation in the panel.
Methodology :
Finite element analysis methodology is used for stress analysis. This is one of the numerical methods of solving structural problems. The aircraft wing landing gear cutout panel is modeled using FEM technique. The analysis is carried out to identify the maximum stress and the location of maximum tensile stress. The refinement of the mesh size is carried out to get mesh independent stress value at critical location.
Fatigue life to crack initiation is carried out at the maximum stress location. S-N curve for the panel material is used for the fatigue life prediction
Accessories used :
The general purpose stress analysis software packages MSC Patran and MSC Nastran are used for stress analysis.
TECHNICAL SKILLS :
- MS Office.
- C Programming.
- Turbo C++.
- CATIA V5R20.
- MSC PATRAN AND MSC NASTRAN.
- SOLIDEDGE V19.
- ANSYS8.
- EXTRA CURRICULAR ACTIVITIES :
- President of an association of Mechanical Engineers “TORQUE” for the year 2009-10.
- Volunteer of many functions conducted in college.
- Volunteered (chief) during a function in which “Dr.APJ Abdul Kalam” visited our college
In the year2009 .
- Presented a paper on “EDDY CURRENT BREAK SYSTEM” under “METAL PRESENTS” held at
DON BOSCO Bangalore.


DECLARATION :
I here by conforming that all the details mentioned above are true and correct to my best of knowledge.
(RAJA. M. DALAL)

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More Information about this submission and submitter :-
___________________________________________________
Submission ID : 4379863
Date & Time : 17th Jul 2011 6:10 AM (UTC)
IP Address : 14.194.60.206
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