This course focuses on aerospace structural analysis and design. Topics include structural components of aircraft, airworthiness and airframe Loads, and analysis of structural components with unsymmetrical cross-sections that are subjected to bending, shear, and torsion in open and closed thin-walled beams, covering single and multi-cell cross-sections. The analysis extends to combined section beams, and structural idealization of critical components like wing spars and ribs and box beams, fuselage, and wings. The course equips students with the skills to analyze and design aerospace structures effectively.