RSS Feed for computational fluid dynamics https://solvonauts.org/%3Faction%3Drss_search%26term%3Dcomputational+fluid+dynamics RSS Feed for computational fluid dynamics 16.100 Aerodynamics (MIT) 16.100 Aerodynamics (MIT) This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub supersonic regimes 16 100 generally has four components subsonic potential flows including source vortex panel methods viscous flows including laminar and turbulent boundary layers aerodynamics of airfoils and wings including thin airfoil theory lifting line theory and panel method interacting boundary layer methods and supersonic and hypersonic airfoil theory Course material varies each year depending upon the focus of the design problem 160 Technical RequirementsFile decompression software such as 160 Winzip 174 160 or 160 StuffIt 174 is required to open the tar files found on this course site 160 MATLAB 1 This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub supersonic regimes 16 100 generally has four components subsonic potential flows including source vortex panel methods viscous flows including laminar and turbulent boundary layers aerodynamics of airfoils and wings including thin airfoil theory lifting line theory and panel method interacting boundary layer methods and supersonic and hypersonic airfoil theory Course material varies each year depending upon the focus of the design problem 160 Technical RequirementsFile decompression software such as 160 Winzip 174 160 or 160 StuffIt 174 is required to open the tar files found on this course site 160 MATLAB 1 http://dspace.mit.edu/handle/1721.1/36884 http://dspace.mit.edu/handle/1721.1/36884 16.100 Aerodynamics (MIT) 16.100 Aerodynamics (MIT) This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub supersonic regimes 16 100 generally has four components subsonic potential flows including source vortex panel methods viscous flows including laminar and turbulent boundary layers aerodynamics of airfoils and wings including thin airfoil theory lifting line theory and panel method interacting boundary layer methods and supersonic and hypersonic airfoil theory Course material varies each year depending upon the focus of the design problem This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub supersonic regimes 16 100 generally has four components subsonic potential flows including source vortex panel methods viscous flows including laminar and turbulent boundary layers aerodynamics of airfoils and wings including thin airfoil theory lifting line theory and panel method interacting boundary layer methods and supersonic and hypersonic airfoil theory Course material varies each year depending upon the focus of the design problem http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-100-aerodynamics-fall-2005 http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-100-aerodynamics-fall-2005 16.100 Aerodynamics (MIT) This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub supersonic regimes 16 100 generally has four components subsonic potential flows including source vortex panel methods viscous flows including laminar and turbulent boundary layers aerodynamics of airfoils and wings including thin airfoil theory lifting line theory and panel method interacting boundary layer methods and supersonic and hypersonic airfoil theory Course material varies each year depending upon the focus of the design problem 160 Technical RequirementsFile decompression software such as 160 Winzip 174 160 or 160 StuffIt 174 is required to open the tar files found on this course site 160 MATLAB 1 https://dspace.mit.edu/handle/1721.1/36884 https://dspace.mit.edu/handle/1721.1/36884 16.100 Aerodynamics (MIT) This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub supersonic regimes 16 100 generally has four components subsonic potential flows including source vortex panel methods viscous flows including laminar and turbulent boundary layers aerodynamics of airfoils and wings including thin airfoil theory lifting line theory and panel method interacting boundary layer methods and supersonic and hypersonic airfoil theory Course material varies each year depending upon the focus of the design problem https://ocw.mit.edu/courses/aeronautics-and-astronautics/16-100-aerodynamics-fall-2005 https://ocw.mit.edu/courses/aeronautics-and-astronautics/16-100-aerodynamics-fall-2005