{"id":6595,"date":"2019-12-14T16:44:29","date_gmt":"2019-12-14T16:44:29","guid":{"rendered":"https:\/\/www.inspirenignite.com\/vtu\/aerospace-propulsion-as-5th-sem-syllabus-for-vtu-be-2017-scheme\/"},"modified":"2019-12-14T16:44:29","modified_gmt":"2019-12-14T16:44:29","slug":"aerospace-propulsion-as-5th-sem-syllabus-for-vtu-be-2017-scheme","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/vtu\/aerospace-propulsion-as-5th-sem-syllabus-for-vtu-be-2017-scheme\/","title":{"rendered":"Aerospace Propulsion AS 5th Sem Syllabus for VTU BE 2017 Scheme"},"content":{"rendered":"

Aerospace Propulsion detail syllabus for Aerospace Engineering (As), 2017 scheme is taken from VTU<\/a> official website and presented for VTU students. The course code (17AS52), 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 as 5th sem syllabus for be 2017 scheme vtu you can visit AS 5th Sem syllabus for BE 2017 Scheme VTU Subjects<\/a>. The detail syllabus for aerospace propulsion is as follows.<\/p>\n

Course Objectives:<\/h4>\n

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

    \n
  1. Understand the working principles of gas turbine and ramjet propulsion systems, the design principles of inlets, combustion chambers, nozzles used in them.<\/li>\n
  2. Learn the operation of compressors and turbines in gas turbine propulsion systems.<\/li>\n
  3. Understand the operation of rocket propulsion<\/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

    Propeller Blade Theory: Momentum theory, Blade element theory, combined blade element and momentum theory, propeller power losses, propeller performance parameters, prediction of static thrust- and in flight, negative thrust, prop fans, ducted propellers, propeller noise, propeller selection, propeller charts.\n<\/p>\n

    Module 3 <\/h4>\n

    Nozzles and Combustion Chamber: Subsonic and supersonic inlets -Relation between minimum area ratio and external deceleration ratio -Starting problem in supersonic inlets -Modes of inlet operation, jet nozzle – Efficiencies – Over expanded, under and optimum expansion in nozzles – Thrust reversal. Classification of Combustion chambers -Combustion chamber performance – Flame tube cooling – Flame stabilization.\n<\/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

    Introduction to rocket propulsion: Introduction to rocket propulsion -Reaction principle – Thrust equation – Classification of rockets based on propellants used – solid, liquid and hybrid – Comparison of these engines with special reference to rocket performance – electric propulsion – classification- electro thermal – electro static -electromagnetic thrusters- geometries of Ion thrusters- beam\/plume characteristics – hall thrusters.\n<\/p>\n

    Course Outcomes:<\/h4>\n

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

      \n
    1. Analyze the engineering concepts of air breathing propulsion systems.<\/li>\n
    2. Distinguish the different types of compressors.<\/li>\n
    3. Choose the propellant based on the application.<\/li>\n<\/ol>\n

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