{"id":58666,"date":"2023-09-05T13:08:13","date_gmt":"2023-09-05T13:08:13","guid":{"rendered":"https:\/\/www.inspirenignite.com\/anna-university\/ae3006-design-of-gas-turbine-engine-components-syllabus-for-aero-2021-regulation-professional-elective-vi\/"},"modified":"2023-09-05T13:08:13","modified_gmt":"2023-09-05T13:08:13","slug":"ae3006-design-of-gas-turbine-engine-components-syllabus-for-aero-2021-regulation-professional-elective-vi","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/anna-university\/ae3006-design-of-gas-turbine-engine-components-syllabus-for-aero-2021-regulation-professional-elective-vi\/","title":{"rendered":"AE3006: Design of Gas Turbine Engine Components syllabus for Aero 2021 regulation (Professional Elective-VI)"},"content":{"rendered":"<p align=\"justify\">Design of Gas Turbine Engine Components detailed syllabus for Aeronautical Engineering (Aero) for 2021 regulation curriculum has been taken from the <a class=\"rank-math-link\" href=\"https:\/\/cac.annauniv.edu\/\" style=\"color: inherit\" target=\"_blank\" rel=\"noopener\">Anna Universities<\/a> official website and presented for the Aero 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<p align=\"justify\">For Aeronautical Engineering 6th Sem scheme and its subjects, do visit <a class=\"rank-math-link\" href=\"..\/aero-6th-sem-syllabus-2021-regulation\">Aero 6th Sem 2021 regulation scheme<\/a>. For Professional Elective-VI scheme and its subjects refer to <a class=\"rank-math-link\" href=\"..\/professional-elective-vi-syllabus-for-aero-2021-regulation\">Aero Professional Elective-VI syllabus scheme<\/a>. The detailed syllabus of design of gas turbine engine components is as follows. <\/p>\n<p><h4>Course Objectives:<\/h4>\n<h4 id=\"istudy\" style=\"text-align:center\"><a class=\"rank-math-link\" href=\"https:\/\/play.google.com\/store\/apps\/details?id=ini.istudy\" style=\"color: inherit\" target=\"_blank\" rel=\"noopener\">Download the iStudy App for all syllabus and other updates.<\/a><br \/><a class=\"rank-math-link\" href=\"https:\/\/play.google.com\/store\/apps\/details?id=ini.istudy&amp;pcampaignid=pcampaignidMKT-Other-global-all-co-prtnr-py-PartBadge-Mar2515-1\/\" target=\"_blank\" rel=\"noopener\"><img decoding=\"async\" src=\"https:\/\/play.google.com\/intl\/en_us\/badges\/static\/images\/badges\/en_badge_web_generic.png\" alt=\"Get it on Google Play\" style=\"height:65px;text-align:center\"><\/a><\/h4>\n<p><h4>Unit I<\/h4>\n<p>GAS TURBINE ENGINE DESIGN FUNDAMENTALS<br \/>\nDesign Process- compressible flow relationship; Constraint Analysis &#8211; Concept-Design tools-preliminary estimates; Mission analysis &#8211; Aircraft weight and fuel consumption data-Example problems on Constrain analysis, Mission analysis.\n<\/p>\n<p><h4>Unit II<\/h4>\n<p>ON DESIGN AND OFF-DESING PARAMETRIC ANALYSIS<br \/>\nTotal and static properties-corrected mass flow rate-Engine Cycle Design- One-Dimensional Through flow Area-Flow path force on components- aircraft constraint analysis, aircraft mission analysis, engine parametric (design point) analysis, engine performance (off-design) analysis, engine installation drag and sizing.\n<\/p>\n<p><h4>Unit III<\/h4>\n<h4 id=\"istudy\" style=\"text-align:center\"><a class=\"rank-math-link\" href=\"https:\/\/play.google.com\/store\/apps\/details?id=ini.istudy\" style=\"color: inherit\" target=\"_blank\" rel=\"noopener\">Download the iStudy App for all syllabus and other updates.<\/a><br \/><a class=\"rank-math-link\" href=\"https:\/\/play.google.com\/store\/apps\/details?id=ini.istudy&amp;pcampaignid=pcampaignidMKT-Other-global-all-co-prtnr-py-PartBadge-Mar2515-1\/\" target=\"_blank\" rel=\"noopener\"><img decoding=\"async\" src=\"https:\/\/play.google.com\/intl\/en_us\/badges\/static\/images\/badges\/en_badge_web_generic.png\" alt=\"Get it on Google Play\" style=\"height:65px;text-align:center\"><\/a><\/h4>\n<p><h4>Unit IV<\/h4>\n<p>COMBUSTION CHAMBER DESIGN<br \/>\nDesign: Combustion system components- Combustion- Chemical reactor theory. Combustor Stability map-Stirring and mixing-Total pressure loss-Fuels-Ignition-Combustion Systems of Main Burner Design: Air partitioning- Main burner component Design: Diffuser-types of burner-inner and outer casing design-Fuel nozzle-Dome and liner-Primary zone- swirler-Secondary holes-Dilution holes-Transition duct-Design of Afterburners-Design parameters-Diffuser-Fuel injectionIgnition-Flame stabilization &#8211; Flame spread and after burner length &#8211; Examples design calculation.\n<\/p>\n<p><h4>Unit V<\/h4>\n<p>INLET AND NOZZLE DESIGN<br \/>\nInlets and Exhaust Nozzles Design: Elements of a Successful Inlet-Engine Integration ProgramDefinition of Subsonic Inlet-Engine Operational Requirements- Definition of Supersonic InletEngine Operational Requirements- Engine Impact on Inlet Design- Inlet Impact on Engine Design-Validation of Inlet-Engine System-Exhaust nozzle design-Nozzle types and their design -Jet control methods for reduction of infrared signature.\n<\/p>\n<p><h4>Course Outcomes:<\/h4>\n<p>Upon completion of this course, Students will be able to<\/p>\n<ol>\n<li>Do preliminary weight and fuel estimation for an aircraft mission.<\/li>\n<li>Identify variation in parametric analysis of ON and OFF design calculations.<\/li>\n<li>Explain the principle design of compressor and turbine and selection of suitable materials.<\/li>\n<li>Estimate the total pressure losses and able to predict ignition delay.<\/li>\n<li>Determine the basic design factors affects ON and OFF design operation of inlets and nozzle on engine performance.<\/li>\n<\/ol>\n<p><h4>Text Books:<\/h4>\n<h4 id=\"istudy\" style=\"text-align:center\"><a class=\"rank-math-link\" href=\"https:\/\/play.google.com\/store\/apps\/details?id=ini.istudy\" style=\"color: inherit\" target=\"_blank\" rel=\"noopener\">Download the iStudy App for all syllabus and other updates.<\/a><br \/><a class=\"rank-math-link\" href=\"https:\/\/play.google.com\/store\/apps\/details?id=ini.istudy&amp;pcampaignid=pcampaignidMKT-Other-global-all-co-prtnr-py-PartBadge-Mar2515-1\/\" target=\"_blank\" rel=\"noopener\"><img decoding=\"async\" src=\"https:\/\/play.google.com\/intl\/en_us\/badges\/static\/images\/badges\/en_badge_web_generic.png\" alt=\"Get it on Google Play\" style=\"height:65px;text-align:center\"><\/a><\/h4>\n<p><h4>Reference Books:<\/h4>\n<ol>\n<li>Cumpsty N., \u201cJet Propulsion: A Simple Guide to the Aerodynamics and Thermodynamics Design and Performance of Jet Engines\u201d , Cambridge University Press; 2nd edition, 2003<\/li>\n<li>Murthy S.N. and Curran E.T.,&#8217; High-Speed Flight Propulsion Systems&#8217;, Volume 137, Progress in Astronautics and Aeronautics, AIAA,1991.<\/li>\n<li>Rathakrish,nan E, &#8216;Applied Gas Dynamics, John Wiley, &amp; Sons (As,ia) Pvt Ltd, 2010. ,<\/li>\n<li>Treage I.E, Aircraft Gas Turbine Engine Technology, 3rd edition, Glencoe McGraw-Hill, Inc. 1995<\/li>\n<\/li>\n<\/ol>\n<p align=\"justify\">For detailed syllabus of all the other subjects of Aeronautical Engineering 6th Sem, visit <a class=\"rank-math-link\" href=\"..\/category\/aero+6th-sem\">Aero 6th Sem subject syllabuses for 2021 regulation<\/a>. <\/p>\n<p align=\"justify\">For all Aeronautical Engineering results, visit <a class=\"rank-math-link\" href=\"https:\/\/www.inspirenignite.com\/anna-university\/anna-university-results\/\">Anna University Aero all semester results<\/a> direct link. <\/p>\n","protected":false},"excerpt":{"rendered":"<p>Design of Gas Turbine Engine Components detailed syllabus for Aeronautical Engineering (Aero) for 2021 regulation curriculum has been taken from the Anna Universities official website and presented for the Aero [&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":[52],"tags":[],"class_list":["post-58666","post","type-post","status-publish","format-standard","hentry","category-aero"],"_links":{"self":[{"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/posts\/58666","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=58666"}],"version-history":[{"count":0,"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/posts\/58666\/revisions"}],"wp:attachment":[{"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/media?parent=58666"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/categories?post=58666"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.inspirenignite.com\/anna-university\/wp-json\/wp\/v2\/tags?post=58666"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}