JNTUK B.Tech Structural Analysis and Detailed Design gives you detail information of Structural Analysis and Detailed Design R13 syllabus It will be help full to understand you complete curriculum of the year.
Course Objective
The main objective of the subject is to make the student to know about the common engineering structures particularly dealt with design of structures for a given loading conditions. Also complete analysis structure worthy to be safe in entire service life. This subject also consider all aircraft structures such as landing gear, wing, fugelage, nose cone etc.
UNIT I : Design Philosophy of aircraft systems, Principles of design, Configuration design, Arriving design specification for detailed design
Design Methodologies: Emphasis on design procedures for the design of wings, fuselage, landing gear, pressure vessels including manevouring loads.
UNIT II : Engineering Design: Design of Aircraft parts and landing gears using engineering design methods/codes and standards to arrive at design for detailed analysis.
Fuselage Design:Loads, effective cross-section, bending strength shearflow analysis. Ultimate strength of stiffend Cylindrical Shells.
UNIT III: Modelling and Simulation Of Wing Surfaces: Estimation of wing loading, wing idelization, mesh generation, element formulation, consistent load vectors, solutions and stress distribution.
UNIT IV: Analysis Of Landing Gear: Evaluation of reaction loads on the members of the landing gear and analysis of lauding gear system, oleo strut, and torque links.
UNIT V: Reliability Based Design: Reliability concepts, bath tub curve, design improvements for reliability.
UNIT VI : Failure Theories: Maximum stress theory, Von Mices theory, Minimum strain energy theory as applicable to aerospace structure and criteria for selection
TEXT BOOKS
- Peery, D.J, and Azar, J.J., Aircraft Structures, 2nd edition, Mc Graw-Hill, N.Y., 1993.
- Rivello, R.M., Theory and Analysis of Flight Structures, McGraw Hill, 1993.
- J.T. Oden, “Mechanics of Elastic Structures”, McGraw-Hill. 1967
- Scheler.E.E and Dunn L.G, “Airplane Structural Analysis and Design”, JohnWiley & Sons.
REFERENCE BOOKS
- Megson, T.M.G., Aircraft Structures for Engineering Students, Edward Arnold, 1985.
- Bruhn. E.H, Analysis and Design of Flight Vehicles Structures, tri -state off set company, USA, 1965. J.T. Oden, “Mechanics of Elastic Structures”, McGrawHill.
- Kuhn.P, “Stressess in Aircraft and Shell Structure”, McGrawHill.
- William.D, “An Introduction to the Theory of Aircraft Structures”, Edward Arnold.
- Kermode.A.C, “The Airplane Structure”, Sir Issacc Pitman Publication.
- Dowty G.H, “Structural Principles and Data”, The new ERA Publishing Cp, 1980.
- Shigley JE, “Mechanical Engineering Design”.
- Pandya & Shah, “Machine Design”
Course Outcomes
At the end of this course, students should be able to
- Get the Knowledge on the most common engineering structures.
- Particularly deal with design of structures for a given loading conditions.
- Analyze structure worthy to be safe in entire service life. This subject also consider all aircraft structures such as landing gear, wing, fugelage, nose cone etc
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