Bhujanga Rao Vakamullu

PROFESSIONAL SUMMARY
-5.0 years of experience in Structural Analysis, Fatigue and Damage Tolerance Analysis of Aircraft Structures using classic Hand Calculation and FEM for metallic and composite structures.
-1.5 years of Sikorsky S-92 Landing Gears, Frames, Skins sizing for Static and Fatigue Analysis (onsite/offshore).
-1.0 years of A320Neo Engine Nacelles Inlet structural analysis experience at Goodrich, Bangalore.
-1.0 years of Bombardier G7000/G8000 series Inboard Flap components (Spars, Flap Tracks and Skins) sizing from conceptual level to the firm design level.
-1.0 years of Airbus A350 XWB winglet ribs fatigue Analysis & Concessions.
-1.0 years of Boeing 787,757 Structural Repairs evaluation by Staic, Fatigue and damage Tolerance Analysis using Boeing Stress Analysis Tools.
-Had Good knowledge in Fatigue and Fracture Mechanics