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JNTU 2007-2008 IV YEAR I SEM. B. TECH. AE -STRUCTURAL ANALYSIS AND DETAILED DESIGN
Posted Date: 09 Dec 2007 Resource Type: Articles/Knowledge Sharing Category: Syllabus
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Posted By: Sri Member Level: Gold
Rating:  Points: 1
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JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY
HYDERABAD
IV Year B. Tech. AE – I semester T P C
4+1* 0 4
STRUCTURAL ANALYSIS AND DETAILED DESIGN
UNIT I
Design Philosophy of aircraft systems
• Principles of design
• Configuration design
• Arriving design specification for detailed design
UNIT II
DESIGN METHODOLOGIES
Emphasis on design procedures for the design of wings, fuselage, landing gear, pressure vessels including manevouring loads.
UNIT III
ENGINEERING DESIGN
Design of Aircraft parts and landing gears using engineering design methods/codes and standards to arrive at design for detailed analysis.
UNIT IV
FUSELAGE DESIGN
Loads, effective cross-section, bending strength shearflow analysis. Ultimate strength of stiffend Cylindrical Shells.
UNIT V
MODELLING AND SIMULATION OF WING SURFACES
Estimation of wing loading, wing idelization, mesh generation, element formulation, consistent load vectors, solutions and stress distribution.
UNIT VI
ANALYSIS OF LANDING GEAR
Evaluation of reaction loads on the members of the landing gear and analysis of lauding gear system, oleo strut, torque links.
UNIT VII
RELIABILITY BASED DESIGN
Reliability concepts, bath tub curve, design improvements for reliability.
UNIT VIII
FAILURE THEORIES
Maximum stress theory, Voin Mices theory, Minimum strain energy theory as applicable to aerospace structure and criteria for selection
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