-More than 4 years of experience in Static, Fatigue and Damage Tolerance Analysis of Aircraft structural parts and along with more than 1 years of experience in designing of aircraft flight test parts.
-Having hands on experience in static analysis of aircraft interiors.
-Worked extensively with parts manufactured with Aluminum (2XXX, 6XXX & 7XXX series) and Steel (321 CRES, 15-5 PH, 17-5 PH & more).
-Expertise in creating design with CATIA V5.
-Expert in handling strength check on the repair accomplished in the Aluminium material using rivets and bolts.
-Good theoretical knowledge on mechanical behavior of plates, shells, beams, columns and pressure vessels.
-Good knowledge of Fracture ...