{"id":8864,"date":"2019-12-15T04:53:04","date_gmt":"2019-12-15T04:53:04","guid":{"rendered":"https:\/\/www.inspirenignite.com\/vtu\/elements-of-jet-propulsion-systems-syllabus-for-vtu-be-2017-scheme-open-elective-2\/"},"modified":"2019-12-15T04:53:04","modified_gmt":"2019-12-15T04:53:04","slug":"elements-of-jet-propulsion-systems-syllabus-for-vtu-be-2017-scheme-open-elective-2","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/vtu\/elements-of-jet-propulsion-systems-syllabus-for-vtu-be-2017-scheme-open-elective-2\/","title":{"rendered":"Elements of Jet Propulsion Systems Syllabus for VTU BE 2017 Scheme (Open Elective-2)"},"content":{"rendered":"

Elements of Jet Propulsion Systems detail syllabus for various departments, 2017 scheme is taken from VTU<\/a> official website and presented for VTU students. The course code (17AS663\/17AE663), 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 open elective-2 syllabus for vtu be 2017 scheme you can visit Open Elective-2 syllabus for VTU BE 2017 Scheme Subjects<\/a>. The detail syllabus for elements of jet propulsion systems is as follows.<\/p>\n

Course Objectives:<\/h4>\n

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

    \n
  1. Understand the basic principle and theory of aircraft propulsion.<\/li>\n
  2. Understand the purpose of a centrifugal, axial compressors, axial and radial turbines<\/li>\n
  3. Acquire knowledge of importance of nozzles & inlets and combustion chamber<\/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
    \n<\/h4>\n

    Propeller Theories & Jet propulsion Types of propeller, Propeller thrust: momentum theory, Blade element theories, propeller blade design, propeller selection.
    \nJet Propulsion: Illustration of working of gas turbine engine – The thrust equation – Factors affecting thrust – Effect of pressure, velocity
    \nand temperature changes of air entering compressor – Methods of thrust augmentation – Characteristics of turboprop, turbofan and turbojet -Performance characteristics.\n<\/p>\n

    Module 3 <\/h4>\n

    Inlets & Nozzles Internal flow and Stall in Subsonic inlets, Boundary layer separation. Major features of external flow near a subsonic inlet. Relation between minimum area ratio and eternal deceleration ratio. Diffuser performance. Supersonic inlets: Supersonic inlets, starting problem in supersonic inlets, Shock swallowing by area variation, External deceleration. Modes of inlet operation. Nozzles: Theory of flow in isentropic nozzles, Convergent nozzles and nozzle choking, Nozzle throat conditions. Nozzle efficiency, Losses in nozzles. Over-expanded and under-expanded nozzles, Ejector and variable area nozzles, Thrust reversal.\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

    Combustion chambers and Turbines Classification of combustion chambers, important factors affecting combustion chamber design, Combustion process, Combustion chamber performance Effect of operating variables on performance – Flame tube cooling – Flame stabilization – Use of flame holders Axial Flow Turbines: Introduction, Turbine stage, Multi-staging of turbine, Exit flow conditions, Turbine cooling, Heat transfer in turbine cooling. Radial turbine: Introduction, Thermodynamics of radial turbines, Losses and efficiency.\n<\/p>\n

    Course Outcomes:<\/h4>\n

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

      \n
    1. Apply the basic principle and theory of aircraft propulsion.<\/li>\n
    2. Explain the functions of centrifugal, axial compressors, axial and radial turbines<\/li>\n
    3. Analyse the performance of nozzles & inlets and combustion chamber<\/li>\n<\/ol>\n

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