{"id":9833,"date":"2020-02-21T14:26:33","date_gmt":"2020-02-21T14:26:33","guid":{"rendered":"https:\/\/www.inspirenignite.com\/vtu\/15an41t-thermodynamics-for-aeronautical-engineering-aero-4th-sem-syllabus-for-diploma-dte-karnataka-c15-scheme\/"},"modified":"2020-02-21T14:26:33","modified_gmt":"2020-02-21T14:26:33","slug":"15an41t-thermodynamics-for-aeronautical-engineering-aero-4th-sem-syllabus-for-diploma-dte-karnataka-c15-scheme","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/vtu\/15an41t-thermodynamics-for-aeronautical-engineering-aero-4th-sem-syllabus-for-diploma-dte-karnataka-c15-scheme\/","title":{"rendered":"15AN41T: Thermodynamics for Aeronautical Engineering Aero 4th Sem Syllabus for Diploma DTE Karnataka C15 Scheme"},"content":{"rendered":"<p>Thermodynamics for Aeronautical Engineering detail DTE Kar Diploma syllabus for Aeronautical Engineering (AE), C15 scheme is extracted from <a href=\"http:\/\/dte.kar.nic.in\/obe11.shtml\/\" target=\"_blank\" rel=\"noopener\">DTE Karnataka<\/a> official website and presented for diploma students. The course code (15AN41T), and for exam duration, Teaching Hr\/week, Practical Hr\/week, Total Marks, internal marks, theory marks, duration and credits do visit complete sem subjects post given below. The syllabus PDFs can be downloaded from official website.<\/p>\n<p>For all other aero 4th sem syllabus for diploma c15 scheme dte karnataka you can visit <a href=\"..\/aero-4th-sem-syllabus-for-diploma-c15-scheme-dte-karnataka\">Aero 4th Sem Syllabus for Diploma C15 Scheme DTE Karnataka Subjects<\/a>. The detail syllabus for thermodynamics for aeronautical engineering is as follows.<\/p>\n<p><h4>Pre-requisites:<\/h4>\n<p>Knowledge of basic mathematics, applied Science and elements of aeronautics\n<\/p>\n<p><h4>Course Objectives:<\/h4>\n<ol>\n<li>Understanding the basic thermodynamics and various cycles (air standard)<\/li>\n<li>This course will provide an understanding of the basic principles of thermodynamics which enables understanding of major fields of Aeronautical engineering system<\/li>\n<\/ol>\n<p><h4>Course Outcomes:<\/h4>\n<p><b>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 Syllabus App<\/a>.<\/b> Its a light weight, easy to use, no images, no pdfs platform to make students life easier.<\/p>\n<p><h4>Course Outcomes:<\/h4>\n<ol>\n<li>CO1\tApply basic concepts, laws and principles of thermodynamics to use in aeronautical applications<\/li>\n<li>CO2\tOutline various thermodynamic processes and analyze them with respect to various parameters<\/li>\n<li>CO3\tUnderstand the limitations, applications and comparison of thermodynamic cycles based on different parameters.<\/li>\n<li>CO4\tApply the learning to calculate various performance parameters of aero engine<\/li>\n<li>CO5\tKnow the fundamentals of heat transfer<\/li>\n<li>CO6\tKnow the classification of gas turbines<\/li>\n<\/ol>\n<p><h4>UNIT I: BASIC CONCEPTS AND LAWS OF THERMODYNAMICS CO1 10 Hrs<br \/>\n<\/h4>\n<p>Basic concepts-Definitions :system &#8211; boundary, surrounding, working fluid and state of a system.-thermodynamic systems &#8211; closed, open and isolated systems with examples-Properties of system- Intensive and Extensive properties with examples.-Definitions for properties like Enthalpy (H), Entropy Internal energy (U)- Specific heat at constant pressure(&#8216;Cp&#8217;), specific heat at constant volume(&#8216;Cv&#8217;) for a gas-Relation between Cp &amp; Cv , characteristic gas equation, Universal gas constant, Definitions for quasi-static work flow-Law of thermodynamics-Zeroth, first &amp; second laws of thermodynamics- simple problems on conversion of Heat into Work and vice versa.-Steady flow energy equation (without proof)\n<\/p>\n<p><h4>UNIT II: THERMODYNAMIC PROCESSES CO2) 10 Hrs<\/p>\n<p><b>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 Syllabus App<\/a>.<\/b> Its a light weight, easy to use, no images, no pdfs platform to make students life easier.<\/p>\n<p><h4>UNIT III: THERMODYNAMIC CYCLES CO3) 10Hrs<br \/>\n<\/h4>\n<p>Thermodynamic cycles &#8211; reversible and irreversible cycles conditions for reversibility of a cycle-Explanation of Carnot cycle with P.V. and T-S diagrams, Air standard Efficiency -Problems on Carnot cycle-Explanation of Otto cycle with P.V. and T-S diagrams, Air standard Efficiency &#8211; Simple problems on Otto cycle-.\n<\/p>\n<p><h4>UNIT IV: AERO ENGINES AND ITS PERFORMANCE CO4. 10Hrs<br \/>\n<\/h4>\n<p>Aero engine -definition-classification- Terminology of engine &#8211; Working principle of Aero engines. Formulae for Brake power, Indicated power Mechanical efficiency, Indicated thermal efficiency, Brake thermal efficiency, Air standard efficiency, Relative efficiency, Volumetric efficiency-\n<\/p>\n<p><h4>UNIT V: ELEMENTS OF HEAT TRANSFER CO5) 06Hrs<\/p>\n<p><b>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 Syllabus App<\/a>.<\/b> Its a light weight, easy to use, no images, no pdfs platform to make students life easier.<\/p>\n<p><h4>UNIT VI: GAS TURBINE AND JET PROPULSION SYSTEMS CO6. 06 Hrs<br \/>\n<\/h4>\n<p>Gas turbines- classification of gas turbines-Closed cycle gas turbine-Schematic diagramexplanation-Open cycle gas turbine-schematic diagram-explanation-Comparison of open cycle and closed cycle gas turbines.-. Explanation of BRAYTON cycle with P.V. and T-S diagrams \u00c2\u00aeTEXT BOOKS AND REFERENCES\n<\/p>\n<p><h4>Reference Books:<\/h4>\n<ol>\n<li>Heat Engines\tPandya and Shah\tCharotar Publishing House<\/li>\n<li>Thermodynamics and Heat power Engg.\tMathur and Mehta\tTata Mcgraw- Hill<\/li>\n<li>A Text book of Thermal Engineering\tR S Khurmi&amp; J K Gupta\tS Chand<\/li>\n<li>Thermal Engineering\tP.L.Ballaney\tKhanna.Publishers<\/li>\n<li>Thermal Engineering\tA. S. Sarao\tSatyaPrakashan<\/li>\n<li>Thermal Engineering\tR K Rajput\tLaxmi.Publications<\/li>\n<li>Practical Thermodynamics\tG D Rai\tKhanna Publisher<\/li>\n<\/ol>\n<p><h4>LIST OF SOFTWARES\/ LEARNING WEBSITES:<\/h4>\n<ol>\n<li>http:\/\/www.nptel.iitm.ac.in\/video.php?subjectId=112105123 (IIT-B Video lectures)<\/li>\n<li>http:\/\/www.thermofluids.net\/<\/li>\n<li>http:\/\/www.grc.nasa.gov\/WWW\/k-12\/airplane\/thermo.html<\/li>\n<li>http:\/\/www.youtube.com\/watch?v=Xb05CaG7TsQ<\/li>\n<li>http:\/\/www.youtube.com\/watch?v=aAfBSJObd6Y<\/li>\n<li>http:\/\/www.youtube.com\/watch?v=DHUwFuHuCdw<\/li>\n<li>http:\/\/www.youtube.com\/watch?v=kJlmRT4E6R0<\/li>\n<li>http:\/\/www.youtube.com\/watch?v=GKqG6n6nAmg<\/li>\n<\/ol>\n<p><h4>Suggested List of Student Activities:<\/h4>\n<\/p>\n<p><i>Note: the following activities or similar activities for assessing CIE (IA) for 5 marks (Any one)<\/i><\/p>\n<ol type=\"i\">\n<li>Each student should do any one of the following type activity or similar activity related to the course and before take up, get it approved from concerned Teacher and HOD.<\/li>\n<li>Each student should conduct different activity and no repeating should occur<\/li>\n<\/ol>\n<ol>\n<li>Identify and list real situations which works on: a: Zeroth law. b: First law of thermodynamics. c: Second law of thermodynamics.<\/li>\n<li>Arrange a visit to any gas turbine power plant, study the operational features of Gas turbines<\/li>\n<\/ol>\n<p><h4>Course Delivery:<\/h4>\n<ul>\n<li>The course will be delivered through lectures and Power point presentations\/ Video<\/li>\n<\/ul>\n<p><h4>Model Question Paper:<\/h4>\n<p>(CIE)<\/p>\n<ol>\n<li>Define the terms:<\/li>\n<ol type=\"i\">\n<li>system<\/li>\n<li>boundary and<\/li>\n<li>surroundings<\/li>\n<\/ol>\n<li>Differentiate between intensive and extensive properties of a system. Give three examples for each<\/li>\n<li>Explain reversible and irreversible process<\/li>\n<p>OR<br \/>\nDraw the PV and TS diagram for<\/p>\n<ol type=\"i\">\n<li>Constant pressure process<\/li>\n<li>Constant volume process<\/li>\n<li>Constant temperature process.<\/li>\n<\/ol>\n<li>A quantity of gas has a volume of &#8216;1.4&#8217; m3, pressure &#8216;5.&#8217; bar and temperature 100oC. If the gas is compressed at a constant pressure, until its volume becomes 1.12 m3, determine :<\/li>\n<ol type=\"i\">\n<li>Temperature at the end of the compression<\/li>\n<li>Work done in compressing the gas<\/li>\n<li>Decrease in internal energy<\/li>\n<li>Heat given out by the gas.<\/li>\n<\/ol>\n<\/ol>\n<p>OR<br \/>\n&#8216;1.&#8217; m3 of air at a pressure of &#8216;5.&#8217; bar is expanded isothermally to &#8216;5.&#8217; m3 calculate the final pressure of the gas and heat supplied during the process.\n<\/ol>\n<\/p>\n<p><h4>Model Question Paper:<\/h4>\n<\/p>\n<p><i>Note: Answer any SIX from PartA and any SEVEN from Part B<\/i><\/p>\n<p><b>PART-A\t6&#215;5=30 marks<\/b><\/p>\n<ol>\n<li>Define the terms:<\/li>\n<ol type=\"i\">\n<li>system<\/li>\n<li>boundary and<\/li>\n<li>surroundings.<\/li>\n<\/ol>\n<li>A closed system received a heat transfer of 120 kJ and delivers a work transfer of 150 kJ. Calculate the change of internal energy.<\/li>\n<li>Derive expression for work done in constant temperature process with PV diagram.<\/li>\n<li>Explain various modes of heat transfer<\/li>\n<li>Give the assumptions made in thermodynamic air standard cycle.<\/li>\n<li>Define AERO engine and give the classification.<\/li>\n<li>Explain following terms:<\/li>\n<ol type=\"i\">\n<li>Volumetric efficiency<\/li>\n<li>Mechanical efficiency<\/li>\n<\/ol>\n<li>Explain the working principle of gas turbine engine.<\/li>\n<li>State the applications and limitations of gas turbine.<\/li>\n<\/ol>\n<p><b>PART-B<\/b><\/p>\n<ol>\n<li><\/li>\n<ol type=\"i\">\n<li>Differentiate between intensive and extensive properties of a system. Give three examples for each. 04<\/li>\n<li>Explain the laws of thermodynamics\t06<\/li>\n<\/ol>\n<li><\/li>\n<ol type=\"i\">\n<li>Prove that Cp- Cv=R 04<\/li>\n<li>Explain with P-V and T-S diagram the Constant pressure, Constant volume,\t06<\/li>\n<\/ol>\n<li><\/li>\n<ol type=\"i\">\n<li>Give the thermodynamic processes on gases. and explain Isothermal, Isentropic, polytrophic process 10<\/li>\n<\/ol>\n<li><\/li>\n<ol type=\"i\">\n<li>Derive an expression for work done during polytrophic process. 04<\/li>\n<li>A gas of mass 5.6 kg is expanded adiabatically from a pressure at 8 bar to 1 bar adiabatically. Initial temperature of the gas is 200oC. Find the work done and change in internal energy. Take Cp = 1 kJ\/kg K and Cv= 7.14 kJ\/kg K.\t06<\/li>\n<\/ol>\n<li>Explain with the help of P-V and T-S diagrams working of Otto cycle and derive an expression for the air standard efficiency of it.\t10<\/li>\n<li>Explain the classification of aero engines and their applications\t10<\/li>\n<li><\/li>\n<ol type=\"i\">\n<li>Define a heat engine. Write a note on air standard efficiency 04<\/li>\n<li>A heat engine has a piston diameter of 150 mm, length of stroke 400 mm and mean effective pressure &#8216;5.&#8217; bar. The engine makes 120 explosions per minute. Determine the mechanical efficiency of the engine, if the engine BP is 5 kW.\t06<\/li>\n<\/ol>\n<li>Define : Brake power, Indicated power Mechanical efficiency, Indicated thermal efficiency, Brake thermal efficiency,\t10<\/li>\n<li><\/li>\n<ol type=\"i\">\n<li>Define :<\/li>\n<ol type=\"a\">\n<li>Conduction<\/li>\n<li>Radiation.<\/li>\n<li>Convection\t3<\/li>\n<\/ol>\n<li>Explain Thermal Radiation, Absorptivity, Transmissivity, Reflectivity, Emissivity,\t7<\/li>\n<\/ol>\n<li><\/li>\n<ol type=\"i\">\n<li>Explain closed cycle gas turbine with schematic diagram. 06<\/li>\n<li>State the applications and limitations of gas turbine 04<\/li>\n<\/ol>\n<\/ol>\n<p>For detail syllabus of all other subjects of BE Aero, C15 scheme do visit <a href=\"..\/category\/aero-diploma+4th-sem\">Aero 4th Sem syllabus for C15 scheme<\/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 Syllabus App<\/a> for latest syllabus and results, class timetable and more.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Thermodynamics for Aeronautical Engineering detail DTE Kar Diploma syllabus for Aeronautical Engineering (AE), C15 scheme is extracted from DTE Karnataka official website and presented for diploma students. The course code [&hellip;]<\/p>\n","protected":false},"author":2298,"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":[5,49],"tags":[],"class_list":["post-9833","post","type-post","status-publish","format-standard","hentry","category-4th-sem","category-aero-diploma"],"_links":{"self":[{"href":"https:\/\/www.inspirenignite.com\/vtu\/wp-json\/wp\/v2\/posts\/9833","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.inspirenignite.com\/vtu\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/www.inspirenignite.com\/vtu\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/www.inspirenignite.com\/vtu\/wp-json\/wp\/v2\/users\/2298"}],"replies":[{"embeddable":true,"href":"https:\/\/www.inspirenignite.com\/vtu\/wp-json\/wp\/v2\/comments?post=9833"}],"version-history":[{"count":0,"href":"https:\/\/www.inspirenignite.com\/vtu\/wp-json\/wp\/v2\/posts\/9833\/revisions"}],"wp:attachment":[{"href":"https:\/\/www.inspirenignite.com\/vtu\/wp-json\/wp\/v2\/media?parent=9833"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.inspirenignite.com\/vtu\/wp-json\/wp\/v2\/categories?post=9833"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.inspirenignite.com\/vtu\/wp-json\/wp\/v2\/tags?post=9833"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}