{"id":6559,"date":"2019-12-14T16:44:08","date_gmt":"2019-12-14T16:44:08","guid":{"rendered":"https:\/\/www.inspirenignite.com\/vtu\/aircraft-performance-aero-6th-sem-syllabus-for-vtu-be-2017-scheme\/"},"modified":"2019-12-14T16:44:08","modified_gmt":"2019-12-14T16:44:08","slug":"aircraft-performance-aero-6th-sem-syllabus-for-vtu-be-2017-scheme","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/vtu\/aircraft-performance-aero-6th-sem-syllabus-for-vtu-be-2017-scheme\/","title":{"rendered":"Aircraft Performance Aero 6th Sem Syllabus for VTU BE 2017 Scheme"},"content":{"rendered":"

Aircraft Performance detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU<\/a> official website and presented for VTU students. The course code (17AE63), 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 6th sem syllabus for be 2017 scheme vtu you can visit Aero 6th Sem syllabus for BE 2017 Scheme VTU Subjects<\/a>. The detail syllabus for aircraft performance is as follows.<\/p>\n

Course Objectives:<\/h4>\n

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

    \n
  1. Understand the aircraft performance in steady unaccelerated and accelerated flight.<\/li>\n
  2. Understand the airplane performance parameters.<\/li>\n
  3. Acquire the knowledge on aircraft maneuver performance.<\/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

    Steady Performance – Level Flight, Climb & Glide Performance: Equation of motion for Rate of climb- graphical and analytical approach -Absolute ceiling, Service ceiling, Time to climb – graphical and analytical approach, climb performance graph (hodograph diagram); maximum climb angle and rate of climb Gliding flight, Range during glide, minimum rate of sink and shallowest angle of glide.\t\t\t\t<\/p>\n

    Module 3 <\/h4>\n

    Fundamental Airplane Performance Parameters The fundamental Parameters: Thrust – to – weight ratio, Wing loading, Drag polar, and lift-to – drag ratio. Minimum velocity. Aerodynamic relations associated with lift-to-drag ratio. Range and Endurance: Propeller driven Airplane: Physical consideration, Quantitative formulation, Breguet equation for Range and Endurance, Conditions for maximum range and endurance. Jet Airplane: Physical consideration, Quantitative formulation, Equation for Range and Endurance, Conditions for maximum range and endurance, Effect\t\t\t\t<\/p>\n

    of head wind tail wind.\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

    Maneuver Performance Turning performance: Level turn, load factor, Constraints on load factor, Minimum turn radius, Maximum turn rate. Pull-up and Pulldown maneuvers: (Turning rate, turn radius). Limiting case for large load factor. The V-n diagram. Limitations of pull up and push over.\t<\/p>\n

    Course Outcomes:<\/h4>\n

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

      \n
    1. Apply the basic airplane performance parameters.<\/li>\n
    2. Differentiate the aircraft performance in steady unaccelerated and accelerated flight.<\/li>\n
    3. Explain the aircraft maneuver performance.<\/li>\n<\/ol>\n

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