{"id":57789,"date":"2023-09-02T16:48:49","date_gmt":"2023-09-02T16:48:49","guid":{"rendered":"https:\/\/www.inspirenignite.com\/anna-university\/cme386-gas-dynamics-and-jet-propulsion-syllabus-for-mae-2021-regulation-professional-elective-vi\/"},"modified":"2023-09-02T16:48:49","modified_gmt":"2023-09-02T16:48:49","slug":"cme386-gas-dynamics-and-jet-propulsion-syllabus-for-mae-2021-regulation-professional-elective-vi","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/anna-university\/cme386-gas-dynamics-and-jet-propulsion-syllabus-for-mae-2021-regulation-professional-elective-vi\/","title":{"rendered":"CME386: Gas Dynamics and Jet Propulsion syllabus for MAE 2021 regulation (Professional Elective-VI)"},"content":{"rendered":"

Gas Dynamics and Jet Propulsion detailed syllabus for Mechanical & Automation Engineering (MAE) for 2021 regulation curriculum has been taken from the Anna Universities<\/a> official website and presented for the MAE students. For course code, course name, number of credits for a course and other scheme related information, do visit full semester subjects post given below. <\/p>\n

For Mechanical & Automation Engineering 6th Sem scheme and its subjects, do visit MAE 6th Sem 2021 regulation scheme<\/a>. For Professional Elective-VI scheme and its subjects refer to MAE Professional Elective-VI syllabus scheme<\/a>. The detailed syllabus of gas dynamics and jet propulsion is as follows. <\/p>\n

Course Objectives:<\/h4>\n

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Unit I<\/h4>\n

BASIC CONCEPTS AND ISENTROPIC FLOWS\t9<\/strong>
\nEnergy and momentum equations of compressible fluid flows, Concepts of compressible flow – Mach waves and Mach cone. Flow regimes, effect of Mach number on compressibility. Stagnation, static, critical properties and their interrelationship. Isentropic flow and its relations. Isentropic flow through variable area ducts -nozzles and diffusers. Use of Gas tables.\n<\/p>\n

Unit II<\/h4>\n

COMPRESSIBLE FLOW THROUGH DUCTS\t9<\/strong>
\nFlows through constant area ducts with heat transfer (Rayleigh flow) and Friction (Fanno flow) – variation of flow properties. Choking. Isothermal flow with friction. Use of Gas tables.\n<\/p>\n

Unit III<\/h4>\n

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Unit IV<\/h4>\n

JET PROPULSION\t9
\nTheory of jet propulsion – thrust equation – Performance parameters – thrust, power and efficiency. Operation, cycle analysis and performance of ram jet, turbojet, turbofan, turbo prop and pulse jet engines.\n<\/p>\n

Unit V<\/h4>\n

SPACE PROPULSION\t9<\/strong>
\nTypes of rocket engines and propellants. Characteristic velocity – thrust equation. Theory of single and multistage rocket propulsion. Liquid fuel feeding systems. Solid propellant geometries. Orbital and escape velocity. Rocket performance calculations.\n<\/p>\n

Course Outcomes:<\/h4>\n

At the end of the course the students would be able to<\/p>\n