units
MAE3401
Faculty of Engineering
Monash home | About Monash | Faculties | Campuses | Contact Monash |
Staff directory | A-Z index | Site map |
6 points, SCA Band 2, 0.125 EFTSLRefer to the specific census and withdrawal dates for the semester(s) in which this unit is offered.
SynopsisThis unit develops further the students' physical understanding and analytical skills by including compressibility effects and the viscous nature of aerodynamic flows and translates that into the ability to formulate, analyse and solve very general aerodynamic problems. It covers control volume analysis of steady, one-dimensional, linear and nonlinear compressible flows. Nozzle flows. Steady, supersonic, two-dimensional linear and nonlinear flows. Linearized compressible subsonic and supersonic flow. Introduction to transonic and hypersonic flow. Control volume analysis of viscous incompressible flow, boundary layer flow and free shear flows like jets and wakes, including momentum integral analysis, similarity analysis and similarity solutions of these equations as they pertain to wall bounded and free shear flows. Application of this knowledge to simple design problems. Objectives
Assessment
Continuous assessment comprising problem sets, assignments and laboratory reports worth 30%, Examination worth 70%. Chief examiner(s)Contact hours36 lectures, 24 hours of problem solving classes and laboratory sessions. PrerequisitesCo-requisitesNone Prohibitions |