{"ModuleCode":"ME3232","ModuleTitle":"Compressible Flow","Department":"Mechanical Engineering","ModuleCredit":"4","Prerequisite":"ME2135","Preclusion":"ME3231","ExamDate":"2015-04-28T13:00+0800","ExamDuration":"P2H","ExamVenue":"E1-06-03/04","Types":["Module"],"Lecturers":["Lim Tee Tai","Estruch Samper, David"],"IVLE":[{"Announcements":null,"Forums":[],"Workbins":[],"Webcasts":[],"Gradebooks":[],"Polls":[],"Multimedia":[],"LessonPlan":[],"ID":"92198751-bc83-4263-acba-83a6416b9fe3","CourseLevel":"1","CourseCode":"ME3232","CourseName":"COMPRESSIBLE FLOW","CourseDepartment":"","CourseSemester":"Semester 2","CourseAcadYear":"2014/2015","CourseOpenDate":"/Date(1420041600000+0800)/","CourseOpenDate_js":"2015-01-01T00:00:00","CourseCloseDate":"/Date(1431187140000+0800)/","CourseCloseDate_js":"2015-05-09T23:59:00","CourseMC":"0","isActive":"N","Permission":"S","Creator":{"UserID":null,"Name":"Lim Tee Tai","Email":null,"Title":null,"UserGuid":"657ef531-6672-424b-af13-2a6d0b25892d","AccountType":null},"hasGradebookItems":true,"hasTimetableItems":true,"hasGroupsItems":false,"hasClassGroupsForSignUp":false,"hasGuestRosterItems":false,"hasClassRosterItems":true,"hasWeblinkItems":true,"hasLecturerItems":true,"hasDescriptionItems":true,"hasReadingItems":true,"hasAnnouncementItems":false,"hasProjectGroupItems":false,"hasProjectGroupsForSignUp":false,"hasConsultationItems":false,"hasConsultationSlotsForSignUp":false,"hasLessonPlanItems":false,"Badge":0,"BadgeAnnouncement":0,"WebLinks":[{"ID":"f5390d31-466e-4037-bfb3-8aeb83dd2eeb","URL":"http://www.dept.aoe.vt.edu/~devenpor/aoe3114/calc.html","Description":"Calculator for ISENTROPIC FLOW, NORMAL AND OBLIQUE SHOCK, FANNO FLOW, and RAYLEIGH FLOW ","Order":1,"Rating":0,"SiteType":null},{"ID":"eb70639f-8abb-454a-84bc-62b4b36c6128","URL":"http://soliton.ae.gatech.edu/people/lsankar/AE3021/Prandtl.Meyer.Function.htm","Description":"Calculator for PRANDTL MEYER EXPANSION FAN ","Order":2,"Rating":0,"SiteType":null}],"Lecturers":[{"ID":"420c7e4b-3b9e-4c70-9fc3-f7276a59f60a","User":{"UserID":null,"Name":"Lim Tee Tai","Email":null,"Title":null,"UserGuid":"657ef531-6672-424b-af13-2a6d0b25892d","AccountType":null},"Role":"Lecturer ","Order":1,"ConsultHrs":null},{"ID":"a41fcf85-ab6d-4ff0-9bcc-6333be3a78f0","User":{"UserID":null,"Name":"Estruch Samper, David","Email":null,"Title":null,"UserGuid":"f9e54aa1-97af-49b7-9d83-277eb501aafd","AccountType":null},"Role":"Co-Lecturer ","Order":2,"ConsultHrs":null}],"Descriptions":[{"ID":"1e5f053b-8835-4692-be49-41f07234cfff","Title":"Learning Outcomes","Description":"The objective of this course is to provide students with basic understanding of the principles of gas dynamics in subsonic and supersonic flow. Upon completion of this module, students should be able to analyse a broad range of compressible flow situations.","Order":1},{"ID":"2e5f053b-8835-4692-be49-41f07234cfff","Title":"Prerequisites","Description":"ME2135 (Fluid Mechanics II)","Order":2},{"ID":"3e5f053b-8835-4692-be49-41f07234cfff","Title":"Teaching Modes","Description":"1. Lectures.
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\r\nEvery Wednesday (14:00 to 16:00 hours)
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\r\n
\r\nPart 2 (David Estruch-Samper): Flow with heat interaction: Rayleigh line flow. Isothermal flow with friction in a constant area duct. Flow with mass interaction. Generalized steady, one-dimensional compressible flow. Method of characteristics for two-dimensional supersonic flows. Characteristic lines and compatibility equations. Supersonic nozzle design. Linearized subsonic and supersonic flow. Introduction to hypersonic flow. Newtonian and modified Newtonian Theory. Mach number independence.","Order":6},{"ID":"8e5f053b-8835-4692-be49-41f07234cfff","Title":"Assessment","Description":"1. Final Examination: 70%
\r\n
\r\n2. Continuous Assessments: 30%
\r\n Part 1: Quiz (15%)
\r\n Part 2: Assignments (15%)
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