JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD

Overview

1, 2. Introduction to the features and application of any one of the professional software employed in modelling and analysis of aircraft structures.

Modeling, Analysis (Maximum Stresses, Deflections) and Code Development, Of Structural Elements under Arbitrary Static Loading - Validation of Solutions with Professional Software

• 3. Bending of uniform cantilever beams.
• 4. Compressive strength of rectangular stiffened plane panels of uniform cross-section.
• 5. Shear and torsion of stiffened thin walled open and closed sections.
• 6. Statically indeterminate trusses.
• 7. Free vibrations of uniform cantilever beams- determination of natural frequencies and mode shapes. Modeling and Analysis of Simple Aircraft Components Using Professional Software
• 8. 3 dimensional landing gear trusses.
• 9. Tapered wing box beams.
• 10. Fuselage bulkheads. Suggested software: ANSYS NASTRAN PATRAN R16 B.TECH AERONAUTICAL ENGG.