{"id":6572,"date":"2019-12-14T16:44:15","date_gmt":"2019-12-14T16:44:15","guid":{"rendered":"https:\/\/www.inspirenignite.com\/vtu\/flight-vehicle-design-aero-8th-sem-syllabus-for-vtu-be-2017-scheme\/"},"modified":"2019-12-14T16:44:15","modified_gmt":"2019-12-14T16:44:15","slug":"flight-vehicle-design-aero-8th-sem-syllabus-for-vtu-be-2017-scheme","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/vtu\/flight-vehicle-design-aero-8th-sem-syllabus-for-vtu-be-2017-scheme\/","title":{"rendered":"Flight Vehicle Design Aero 8th Sem Syllabus for VTU BE 2017 Scheme"},"content":{"rendered":"

Flight Vehicle Design detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU<\/a> official website and presented for VTU students. The course code (17AE82), 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 8th sem syllabus for be 2017 scheme vtu you can visit Aero 8th Sem syllabus for BE 2017 Scheme VTU Subjects<\/a>. The detail syllabus for flight vehicle design is as follows.<\/p>\n

Course Objectives:<\/h4>\n

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

    \n
  1. Comprehend the flight vehicle design process.<\/li>\n
  2. Acquire the knowledge of vehicle configuration and structural components.<\/li>\n
  3. Understand the stability & control and subsystems.<\/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

    Configuration Layout & loft: Conic Lofting, Conic Fuselage Development, Conic Shape Parameter, Wing-Tail Layout & Loft. Aerofoil Linear Interpolation. Aerofoil Flat-wrap Interpolation. Wing aerofoil layout-flap wrap. Wetted area determination. Special considerations in Configuration Layout: Aerodynamic, Structural, Detectability. Crew station, Passenger, and Payload arrangements. Design of Structural Components: Fuselage, Wing, Horizontal & Vertical Tail. Spreadsheet for fuselage design. Tail arrangements, Horizontal & Vertical Tail Sizing. Tail Placement. Loads on Structure. V-n Diagram, Gust Envelope. Loads distribution, Shear and Bending Moment analysis.\t<\/p>\n

    Module 3 <\/h4>\n

    Engine Selection & Flight Vehicle Performance Turbojet Engine Sizing, Installed Thrust Correction, Spread Sheet for Turbojet Engine Sizing. Propeller Propulsive System. Propeller design for cruise. Take-off, Landing & Enhanced Lift Devices :- Ground Roll, Rotation, Transition, Climb, Balanced Field Length, Landing Approach, Braking, Spread Sheet for Take-off and Landing. Enhanced lift design -Passive & Active. Spread Sheet\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

    Design Aspects of Subsystems Flight Control system, Landing Gear and subsystem, Propulsion and Fuel System Integration, Air Pressurization and Air Conditioning System, Electrical & Avionic Systems, Structural loads, Safety constraints, Material selection criteria.\t<\/p>\n

    Course Outcomes:<\/h4>\n

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

      \n
    1. Calculate the thrust to weight ratio and wing loading.<\/li>\n
    2. Compute the flight vehicle performance.<\/li>\n
    3. Select the subsystems as per vehicle design.<\/li>\n<\/ol>\n

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