Rahul C.R is seeking an opportunity as a structural engineer in the aviation field. He has over 2 years of experience in stress analysis and design. He has skills in CAD, CAE, and PDM/PLM tools. His projects include structural analysis, optimization, and weight reduction of aircraft components. Rahul holds a B.E in Aeronautical Engineering and has good communication and problem-solving abilities.

1. RESUME
RAHUL C.R Email ID : crrahul0306@gmail.com
CHOMATTIL (H), Mobile : 8147449564
THALORE (P.O), Home : 9995902705
THRISSUR, KERALA.
Career Profile:
A highly ambitious, skilled and knowledgeable structural Engineer with extensive
knowledge in STRESS ANALYSIS and DESIGN field looking for an opportunity in the
aviation field as an acknowledged engineer in a renowned organization.
Professional Strengths:
 Possess excellent verbal and written communication skills
 Quick learner and ability to work under pressure
 Ample knowledge in propulsion, aircraft structure and FEA
 Self-motivated and determined
 Ability to handle multiple tasks
SOFTWARE SKILLS
 CAD PACKAGES : Catia V20, AUTOCAD 2013.
 CAE PACKAGES : HYPERMESH 11.0, NASTRAN PATRAN 2013.
 PDM/PLM TOOLS : TEAM CENTER 9.0.
Work Experience:
TOTAL YEAR OF EXPERIENCE - 2 year and 1 month
Company : LEADAWARD INDIA PVT.LTD (Duration: 5 month
(4/June/2013 to 20/October/2013)
Designation : trainee engineer.
Company : HINDUSTAN AERONAUTICS LIMITED (Duration: 1 year
(21/OCT/2013 TO 20/OCT/2014)
Designation : Graduate Trainee at STRESS DEPARTMENT of ARDC division.
Company : SKYLAB TECHNOLOGIES PVT.LTD (period: from November 2014)
Designation : Stress engineer.

2. PROJECTS INVOLVED IN:
Project Title 1: OPTIMIZATION AND DESIGN OF COMPOSITE FUSELAGE STRUCTURES
OF L.C.A A/C.
Software : Catia, Nastran and patran and hypermesh.
Description : Finite element modelling of fuselage structure and load calculation of
various members whether it will meet the design requirement by applying the loads and
boundary conditions to the structures.
Project Title 2: WEIGHT REDUCTION OF LANDING GEAR FRONT AND AFTER SPAR
OF HTT-40 A/C.
Software : Nastran and Patran.
Description : Finite element modelling of front and after spar by using 3-D element.
Proper boundary conditions and loads were applied on that model for two critical load cases and
analysed the model for optimizing the part for maximum material conservation and high strength
consideration.
Project Title 3: STRUCTURAL ANALYSIS OF FUSELAGE TO WING LUG ATTACHMENT
of L.C.A aircraft.
Software : Nastran and Patran
Description : Proper modelling of lug by U.G software from N.M.G data, proper
meshing and loads and boundary conditions were applied on that model for different load
cases by using bush elements, compare the results with lug failure checks.
Project Title 4: BUCKLING ANALYSIS OF WING SKIN ON A PANCHI U.A.V AIRCRAFT.
Description : proper modelling of wing skin of panchi type u.a.v aircraft from NM.G
data. Proper meshing and boundary conditions and loads are applied on that model and
finished the analysis by composite analysis basis.
Software : Hyper mesh and Nastran patran

3. Educational Summary:
Personal Details:
 Name : Rahul cr.
 Father Name : Ravi c.v.
 Date of Birth : 21/08/1991.
 Sex : Male
 Nationality : Indian
 Marital status : Single
 Languages Known : English,Hindi,Malayalam, Tamil
 Passport Availability : Yes
Declaration:
I hereby certify that the details furnished above are correct to best of my knowledge.
Kindly consider my application and provide me an opportunity to serve in your esteemed
organization
Yours Faithfully
QUALIFICATION
SCHOOL/
INSTITUTION
BOARD/
UNIVERSITY
YEAR OF
PASSING
PERCENTAGE
OF MARKS
B.E
(Aeronautical
Engineering)
Dhanalakshmi
Srinivasanengineering
college,perambalur
Anna
University,
Chennai.
2013 79%
H.S.C
Govt.nandikkara
highersecondary
school
State Board 2009
80%
S.S.L.C
Deepthi high
school,thalore.
State Board 2007
86 %

4. 22/06/15 (RAHUL C.R)
BANGLORE