{"id":1486,"date":"2016-08-03T10:47:10","date_gmt":"2016-08-03T10:47:10","guid":{"rendered":"http:\/\/www.inspirenignite.com\/jntuk\/?p=1486"},"modified":"2016-08-03T10:47:10","modified_gmt":"2016-08-03T10:47:10","slug":"jntuk-b-tech-aerospace-propulsion-i-for-r13-batch","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/jntuk\/jntuk-b-tech-aerospace-propulsion-i-for-r13-batch\/","title":{"rendered":"JNTUK B. Tech Aerospace Propulsion \u2013 I for R13 Batch."},"content":{"rendered":"<p>JNTUK B.Tech Aerospace Propulsion \u2013 I gives you detail information of Flight Aerospace Propulsion \u2013 I R13 syllabus It will be help full to understand you complete curriculum of the year.<\/p><div class=\"a9916ad81d5189659b0bfae0b37c143c\" data-index=\"1\" style=\"float: none; margin:10px 0 10px 0; text-align:center;\">\n<ins class=\"adsbygoogle\"\r\n     style=\"display:block; text-align:center;\"\r\n     data-ad-layout=\"in-article\"\r\n     data-ad-format=\"fluid\"\r\n     data-ad-client=\"ca-pub-1181153414625576\"\r\n     data-ad-slot=\"9648548092\"><\/ins>\r\n<script>\r\n     (adsbygoogle = window.adsbygoogle || []).push({});\r\n<\/script>\n<\/div>\n\n<p><strong>Course Objective<\/strong><\/p>\n<p>The main objective of the subject is to study the fundamentals of gas turbine engines working principles and thrust equation. Subsonic and Supersonic inlets and modes of their evaluation are also considered. It also includes combustion chambers different types of combustion chambers and performance analysis. The compressors and nozzles of gas turbine are studied.<\/p>\n<p><strong>UNIT -I : Fundamentals Of Gas Turbine Engines:<\/strong> Illustration of working of gas turbine engine &#8211; The thrust equation &#8211; Factors affecting thrust \u2013 Effect of pressure, velocity and temperature changes of air entering compressors \u2013 Method of thrust augmentation \u2013 Characteristics of turboprop, turbojet \u2013 Performance characteristics.<\/p>\n<p><strong>UNIT &#8211; II : Subsonic Inlets :<\/strong> Internal flow and Stall in Subsonic inlets &#8211; Boundary layer separation \u2013 Major features of external flow near a subsonic inlet \u2013 Relation between minimum area ratio and eternal deceleration ratio &#8211; Diffuser performance.<br \/>\n<strong>Supersonic Inlets<\/strong> : Supersonic inlets &#8211; Starting problem in supersonic inlets &#8211; Shock swallowing by area variation- External deceleration \u2013Modes of inlet operation.<\/p>\n<p><strong>UNIT &#8211; III : Combustion Chambers And Performance:<\/strong> Classification of combustion chambers \u2013 Important factors affecting combustion chamber design \u2013 Combustion process\u2013 Combustion chamber performance.<\/p>\n<p><strong>UNIT &#8211; IV : Performance Sensitivity:<\/strong> Effect of operating variables on performance &#8211; Flame tube cooling &#8211; Flame stabilization \u2013 Use of flame holders \u2013Numerical problems.<\/p>\n<p><strong>UNIT &#8211; V : Nozzles: Theory of flow in isentropic nozzles<\/strong> &#8211; Convergent nozzles and nozzle choking \u2013 Nozzle throat conditions \u2013 Nozzle efficiency \u2013 Losses in nozzles \u2013 Over-expanded and under-expanded nozzles &#8211; Ejector and variable area nozzles &#8211; Interaction of nozzle flow with adjacent surfaces \u2013 Thrust reversal.<\/p>\n<p><strong>UNIT &#8211; VI : Centrifugal Compressors:<\/strong> Principle of operation of centrifugal compressors &#8211; Work done and pressure rise -Velocity diagrams &#8211; Diffuser vane design considerations \u2013 Concept of Prewhirl \u2013Rotating stall.<br \/>\n<strong>Axial Flow Compressors:<\/strong> Elementary theory of axial flow compressor \u2013 Velocity triangles \u2013 Degree of reaction &#8211; Three dimensional flow &#8211; Air angle distribution for free vortex and constant reaction designs &#8211; Compressor blade design &#8211; Centrifugal and Axial compressor performance characteristics.<\/p>\n<p><strong>TEXT BOOKS<\/strong><\/p>\n<ul>\n<li>Mathur M L &amp; Sharma R P; Gas Turbines and Jet &amp; Rocket Propulsion, Standard Publisher, Delhi, 2000.<\/li>\n<li>Cohen, H. Rogers, G.F.C. and Saravanamuttoo, H.I.H. Gas Turbine Theory, Longman, ELBSEd, 1989.<\/li>\n<\/ul>\n<p><strong>REFERENCE BOOKS<\/strong><\/p>\n<ul>\n<li>Oates G C, AeroThermodyanamics of Aircraft Engine Components, AIAA Edn. Services, NY, 1986.<\/li>\n<li>Rolls- Royce, Jet Engine, 3rd edition, 1983.<\/li>\n<li>Ganesan V, Gas Turbines, TMGH Pub Co &amp; Ed, Delhi, 1999.<\/li>\n<li>Philipa Hill and Carl Peterson, Mechanics and Thermodynamics of Propulsion, Addison Wesley Longman Inc, 1999.<\/li>\n<\/ul>\n<p><strong>Course Outcomes<\/strong><br \/>\nAt the end of the course the students shall be able to:<\/p>\n<ul>\n<li>Understand the fundamentals of gas turbine engines working principles and thrust equation.<\/li>\n<li>Evaluate Subsonic and Supersonic inlets and modes.<\/li>\n<li>Describe the different types of combustion chambers and performance analysis.<\/li>\n<li>Emphasize the compressors and nozzles of gas turbine.<\/li>\n<\/ul>\n<p>For more information about all JNTU updates please stay connected to us on FB and don\u2019t hesitate to ask any questions in the comment.<\/p>\n<div class=\"a9916ad81d5189659b0bfae0b37c143c\" data-index=\"2\" style=\"float: none; margin:10px 0 10px 0; text-align:center;\">\n<ins class=\"adsbygoogle\"\r\n     style=\"display:block; text-align:center;\"\r\n     data-ad-layout=\"in-article\"\r\n     data-ad-format=\"fluid\"\r\n     data-ad-client=\"ca-pub-1181153414625576\"\r\n     data-ad-slot=\"8060844699\"><\/ins>\r\n<script>\r\n     (adsbygoogle = window.adsbygoogle || []).push({});\r\n<\/script>\n<\/div>\n\n<div style=\"font-size: 0px; height: 0px; line-height: 0px; margin: 0; padding: 0; clear: both;\"><\/div>","protected":false},"excerpt":{"rendered":"<p>JNTUK B.Tech Aerospace Propulsion \u2013 I gives you detail information of Flight Aerospace Propulsion \u2013 I R13 syllabus It will be help full to understand you complete curriculum of the [&hellip;]<\/p>\n","protected":false},"author":2259,"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":[2],"tags":[],"class_list":["post-1486","post","type-post","status-publish","format-standard","hentry","category-syllabus"],"_links":{"self":[{"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/posts\/1486","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/users\/2259"}],"replies":[{"embeddable":true,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/comments?post=1486"}],"version-history":[{"count":1,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/posts\/1486\/revisions"}],"predecessor-version":[{"id":1487,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/posts\/1486\/revisions\/1487"}],"wp:attachment":[{"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/media?parent=1486"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/categories?post=1486"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/tags?post=1486"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}