{"id":16205,"date":"2019-12-10T03:41:51","date_gmt":"2019-12-10T03:41:51","guid":{"rendered":"https:\/\/www.inspirenignite.com\/anna-university\/propulsion-i-aero-4th-sem-syllabus-for-be-2017-regulation-anna-univ\/"},"modified":"2019-12-10T03:41:51","modified_gmt":"2019-12-10T03:41:51","slug":"propulsion-i-aero-4th-sem-syllabus-for-be-2017-regulation-anna-univ","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/anna-university\/propulsion-i-aero-4th-sem-syllabus-for-be-2017-regulation-anna-univ\/","title":{"rendered":"Propulsion I Aero 4th Sem Syllabus for BE 2017 Regulation Anna Univ"},"content":{"rendered":"<p>Propulsion I detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is taken from <a href=\"https:\/\/www.annauniv.edu\/\" target=\"_blank\" rel=\"noopener\">Anna University<\/a> official website and presented for students of Anna University. The details of the course are: course code (AE8404), Category (PC), Contact Periods\/week (5), Teaching hours\/week (3), Practical Hours\/week (2). The total course credits are given in combined syllabus.<\/p>\n<p>For all other aero 4th sem syllabus for be 2017 regulation anna univ you can visit <a href=\"..\/aero-4th-sem-syllabus-for-be-2017-regulation-anna-univ\">Aero 4th Sem syllabus for BE 2017 regulation Anna Univ Subjects<\/a>. The detail syllabus for propulsion i is as follows.&#8221;<\/p>\n<p><h4>Course Objective:<\/h4>\n<ul>\n<li>To establish fundamental approach and application of jet engine components. Also analysis of flow phenomenon and estimation of thrust developed by jet engine.<\/li>\n<\/ul>\n<p><h4>Unit I<\/h4>\n<p>For complete syllabus and results, class timetable and more pls <a href=\"https:\/\/play.google.com\/store\/apps\/details?id=ini.istudy\" target=\"_blank\" rel=\"noopener\">download iStudy<\/a>. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.<\/p>\n<p><h4>Unit II<\/h4>\n<p><strong> Jet Engine Intakes and Exhaust Nozzles<\/strong><br \/>\nRam effect, Internal flow and Stall in subsonic inlets &#8211; relation between minimum area ratio and eternal deceleration ratio &#8211; diffuser performance &#8211; modes of operation &#8211; supersonic inlets -starting problem on supersonic inlets &#8211; shock swallowing by area variation &#8211; real flow through nozzles and nozzle efficiency &#8211; losses in nozzles &#8211; ejector and variable area nozzles &#8211; interaction of nozzle flow with adjacent surfaces &#8211; thrust reversal.\n<\/p>\n<p><h4>Unit III<\/h4>\n<p><strong> Jet Engine Combustion Chambers<\/strong><br \/>\nChemistry of combustion, Combustion equations, Combustion process, classification of combustion chambers &#8211; combustion chamber performance &#8211; effect of operating variables on performance &#8211; flame stabilization, Cooling process, Materials, Aircraft fuels, HHV, LHV, Orsat apparatus\n<\/p>\n<p><h4>Unit IV<\/h4>\n<p>For complete syllabus and results, class timetable and more pls <a href=\"https:\/\/play.google.com\/store\/apps\/details?id=ini.istudy\" target=\"_blank\" rel=\"noopener\">download iStudy<\/a>. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.<\/p>\n<p><h4>Unit V<\/h4>\n<p><strong> Jet Engine Turbines<\/strong><br \/>\nPrinciple of operation of axial flow turbines- limitations of radial flow turbines- Work done and pressure rise &#8211; Velocity diagrams &#8211; degree of reaction &#8211; constant nozzle angle designs -performance parameters of axial flow turbine- turbine blade cooling methods &#8211; stage efficiency calculations &#8211; basic blade profile design considerations &#8211; matching of compressor and turbine\n<\/p>\n<p><h4>Course Outcome:<\/h4>\n<ul>\n<li>To be able to apply control volume and momentum equation to estimate the forces produced by aircraft propulsion systems<\/li>\n<li>To be able to describe the principal figures of merit for aircraft engine<\/li>\n<li>To be able to describe the principal design parameters and constraints that set the performance of gas turbine engines.<\/li>\n<li>To apply ideal and actual cycle analysis to a gas turbine engine to relate thrust and fuel burn to component performance parameters.<\/li>\n<li>Understanding the workings of multistage compressor or turbine, and to be able to use velocity triangles and the Euler Turbine Equation to estimate the performance of a compressor or turbine stage.<\/li>\n<\/ul>\n<p><h4>Text Books:<\/h4>\n<ol>\n<li>Hill, P.G. and Peterson, C.R. Mechanics and Thermodynamics of Propulsion Pearson education (2009)<\/li>\n<\/ol>\n<p><h4>References:<\/h4>\n<ol>\n<li>Cohen, H. Rogers, G.F.C. and Saravanamuttoo, H.I.H. Gas Turbine Theory, Pearson Education Canada; 6th edition, 2008.<\/li>\n<li>Mathur, M.L. and Sharma, R.P., Gas Turbine, Jet and Rocket Propulsion, Standard Publishers and Distributors, Delhi, 2nd edition 2014.<\/li>\n<li>Oates, G.C., Aero thermodynamics of Aircraft Engine Components, AIAA Education Series, New York, 1985.<\/li>\n<li>Rolls Royce Jet Engine, Rolls Royce; 4th revised edition, 1986.<\/li>\n<\/li>\n<\/ol>\n<p>For detail syllabus of all other subjects of BE Aero, 2017 regulation do visit <a href=\"..\/category\/aero+4th-sem\">Aero 4th Sem syllabus for 2017 Regulation<\/a>.<\/p>\n<p>Dont forget to <a href=\"https:\/\/play.google.com\/store\/apps\/details?id=ini.istudy\" target=\"_blank\" rel=\"noopener\">download iStudy<\/a> for latest syllabus and results, class timetable and more.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Propulsion I detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is taken from Anna University official website and presented for students of Anna University. The details of the course are: [&hellip;]<\/p>\n","protected":false},"author":2297,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"_bbp_topic_count":0,"_bbp_reply_count":0,"_bbp_total_topic_count":0,"_bbp_total_reply_count":0,"_bbp_voice_count":0,"_bbp_anonymous_reply_count":0,"_bbp_topic_count_hidden":0,"_bbp_reply_count_hidden":0,"_bbp_forum_subforum_count":0,"footnotes":""},"categories":[47,52],"tags":[],"class_list":["post-16205","post","type-post","status-publish","format-standard","hentry","category-4th-sem","category-aero"],"_links":{"self":[{"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/posts\/16205","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/users\/2297"}],"replies":[{"embeddable":true,"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/comments?post=16205"}],"version-history":[{"count":0,"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/posts\/16205\/revisions"}],"wp:attachment":[{"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/media?parent=16205"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/categories?post=16205"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/tags?post=16205"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}