{"id":22457,"date":"2020-07-15T11:12:45","date_gmt":"2020-07-15T11:12:45","guid":{"rendered":"https:\/\/www.inspirenignite.com\/jntuh\/ae605pc-aerospace-propulsion-lab-aero-syllabus-for-btech-3rd-year-2nd-sem-r18-regulation-jntuh\/"},"modified":"2020-07-15T11:12:45","modified_gmt":"2020-07-15T11:12:45","slug":"ae605pc-aerospace-propulsion-lab-aero-syllabus-for-btech-3rd-year-2nd-sem-r18-regulation-jntuh","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/jntuh\/ae605pc-aerospace-propulsion-lab-aero-syllabus-for-btech-3rd-year-2nd-sem-r18-regulation-jntuh\/","title":{"rendered":"AE605PC: Aerospace Propulsion Lab AERO Syllabus for B.Tech 3rd Year 2nd Sem R18 Regulation JNTUH"},"content":{"rendered":"

Aerospace Propulsion Lab detailed Syllabus for Aeronautical Engineering (AERO), R18 regulation has been taken from the JNTUH<\/a> official website and presented for the students affiliated to JNTUH course structure. For Course Code, Subject Names, Theory Lectures, Tutorial, Practical\/Drawing, Credits, and other information do visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the universities official website.<\/p>\n

For all other AERO 3rd Year 2nd Sem Syllabus for B.Tech R18 Regulation JNTUH, do visit AERO 3rd Year 2nd Sem Syllabus for B.Tech R18 Regulation JNTUH <\/a>Subjects. The detailed Syllabus for aerospace propulsion lab is as follows. <\/p>\n

Pre-requisite:<\/h4>\n

For the complete Syllabus, results, class timetable, and many other features kindly download the iStudy App<\/a>
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier.<\/b>
\"Get<\/a>. <\/p>\n

Course Objectives:<\/h4>\n

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  1. Understand the basics of propulsion, working principles of reciprocating engines, performance estimation based on rotation angles, and components of engine and their functions<\/li>\n
  2. Knowledge about the operation of valves, ports and their functioning in four stroke and two stroke engines.<\/li>\n
  3. Calculation of percentage of carbon residue and flash and fire point temperatures of a Lubricating Oil.<\/li>\n
  4. Understand the basic characteristics and range of performance of axial flow gas turbine. Perform parametric jet engine performance analysis and turbo machinery and basic combustion calculations.<\/li>\n<\/ol>\n

    Course Outcomes:<\/h4>\n

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