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AIRFRAME STRUCTURAL DESIGN - IARE, Best Engineering …

AIRFRAME STRUCTURAL DESIGNCOURSE CODE:A72118IV B. Tech I semesterDepartment of Aeronautical Thraza,Assistant ProfessorMr. Vishal, Assistant ProfessorINSTITUTE OF AERONAUTICAL Engineering (Autonomous)Dundigal, Hyderabad -500 0431 UNIT-IINTRODUCTION AIRWORTHINESS REQUIREMENTS2 BASIC AIRCRAFT STRUCTURE3 Outline of Presentation Aircraft Components Material use in AIRFRAME Construction Example of Material use in AIRFRAME Construction FuselageStructure-Truss Type-Pratt Truss-Warren Truss-Monocoque-Semi-Monocoque Basic Structure Member Terms Wing Structure Empennage Structure Power Plant-Wing Pod Mount-Fuselage Mount Landing Gear or Gear or UndercarriageAircraft Components6 PropellerLanding GearWingLeft AileronFuselageEmpennageNacelleRight AileronWingHorizontal StabilizerVertical StabilizerRudderElevator7 Main body of airplane Pilot & cargo compartments Generally constructed in two or more sections Carries accessories and other equipments Includes numerous access doors, inspection plates, landing wheel wells, and other openingsFuselage8 Airfoils attached to each side of the fuselage Main lifting surfaces Various DESIGN size and shape May be attached at the top.

The goal of structural analysis is to get the efficient structure and verify its fitness for use. Structural analysis is the determination of the effects of loads on physical structures and their components. As a science, structural analysis covers principles and methods of strength, rigidity and stability calculations. 53

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