{"id":6553,"date":"2019-12-14T16:44:05","date_gmt":"2019-12-14T16:44:05","guid":{"rendered":"https:\/\/www.inspirenignite.com\/vtu\/aircraft-structures-i-aero-5th-sem-syllabus-for-vtu-be-2017-scheme\/"},"modified":"2019-12-14T16:44:05","modified_gmt":"2019-12-14T16:44:05","slug":"aircraft-structures-i-aero-5th-sem-syllabus-for-vtu-be-2017-scheme","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/vtu\/aircraft-structures-i-aero-5th-sem-syllabus-for-vtu-be-2017-scheme\/","title":{"rendered":"Aircraft Structures-I Aero 5th Sem Syllabus for VTU BE 2017 Scheme"},"content":{"rendered":"

Aircraft Structures-I detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU<\/a> official website and presented for VTU students. The course code (17AE54), and for exam duration, Teaching Hr\/week, Practical Hr\/week, Total Marks, internal marks, theory marks, duration and credits do visit complete sem subjects post given below.<\/p>\n

For all other aero 5th sem syllabus for be 2017 scheme vtu you can visit Aero 5th Sem syllabus for BE 2017 Scheme VTU Subjects<\/a>. The detail syllabus for aircraft structures-i is as follows.<\/p>\n

Course Objectives:<\/h4>\n

This course will enable students to<\/p>\n

    \n
  1. Comprehend the basic concepts of stress and strain.<\/li>\n
  2. Acquire the knowledge of types of loads on aerospace vehicles.<\/li>\n
  3. Understand the theory of elasticity.<\/li>\n<\/ol>\n

    Module 1 <\/h4>\n

    For complete syllabus and results, class timetable and more pls download iStudy<\/a>. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.<\/p>\n

    Module 2<\/h4>\n

    Design for Impact and Fatigue Strength Impact Strength: Introduction, Impact stresses due to axial, bending and torsional loads, effect of inertia. Fatigue Strength: Introduction, S-N Diagram, Low cycle fatigue, High cycle fatigue, Endurance limit, modifying factors: size effect, surface effect, Stress concentration effects, Fluctuating stresses, Goodman and Soderberg relationship, stresses due to combined loading, cumulative fatigue damage.\t\t\t\t\t<\/p>\n

    Module 3<\/h4>\n

    Loads on Aircraft and Aircraft Materials Loads on Aircraft: Structural nomenclature, Types of loads, load factor, Aerodynamics loads, Symmetric manoeuvre loads, Velocity diagram, Function of structural components.\t\t\t\t\t<\/p>\n

    Aircraft Materials: Metallic and non-metallic materials, Use of Aluminum alloy, titanium, stainless steel and composite materials.\t\t\t\t\t<\/p>\n

    Desirable properties for aircraft application. Fracture and Fatigue, Stress Intensity Factor, Crack Growth Rate Derivation.\t\t<\/p>\n

    Module 4 <\/h4>\n

    For complete syllabus and results, class timetable and more pls download iStudy<\/a>. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.<\/p>\n

    Module 5 <\/h4>\n

    Energy Methods and Columns Energy Methods: Strain Energy due to axial, bending and Torsional loads. Castigliano’s theorem, Maxwell’s Reciprocal theorem. Columns: Columns with various end conditions, Euler’s Column curve, Rankine’s formula, Column with initial curvature, Eccentric loading, south-well plot, Beam-column.\t<\/p>\n

    Course Outcomes:<\/h4>\n

    After studying this course, students will be able to:<\/p>\n

      \n
    1. Apply the basic concepts of stress and strain analysis.<\/li>\n
    2. Compute the impact stress.<\/li>\n
    3. Identify appropriate materials for suitable application based on properties.<\/li>\n<\/ol>\n

      Graduate Attributes (as per NBA):<\/h4>\n