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AIRFRAME STRUCTURAL DESIGN

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

1940-1950. Sweptback wings, thick stressed skin, thin-walled beam structure. Mikoyan-Gurevich MiG-15, Soviet Union, 1949 Take-off mass 4 917 kg, wingspan 10 m 45. HISTORICAL PROGRESS OF AIRCRAFT STRUCTURES ... Design model Results of analysis Implementation on real object 55. FLOWCHART OF STRUCTURAL ANALYSIS Real object …

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