https://solvonauts.org/%3Faction%3Drss_search%26term%3Dsubsonic RSS Feed for subsonic 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 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 The course begins with the basics of compressible fluid dynamics including governing equations thermodynamic context and characteristic parameters The next large block of lectures covers quasi one dimensional flow followed by a discussion of disturbances and unsteady flows The second half of the course comprises gas dynamic discontinuities including shock waves and detonations and concludes with another large block dealing with two dimensional flows both linear and non linear The course begins with the basics of compressible fluid dynamics including governing equations thermodynamic context and characteristic parameters The next large block of lectures covers quasi one dimensional flow followed by a discussion of disturbances and unsteady flows The second half of the course comprises gas dynamic discontinuities including shock waves and detonations and concludes with another large block dealing with two dimensional flows both linear and non linear http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-120-compressible-flow-spring-2003 http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-120-compressible-flow-spring-2003 Between 2014 and June 2015 China conducted four major tests of its hypersonic missiles with a fifth test in August The fourth test of Wu 14 its ultra high speed nuclear delivery vehicle demonstrated a capacity for extreme maneuvers It was assessed as travelling at a speed of Mach 10 flying at 10 times the speed of sound or approximately 7 680 miles per hour To understand this in comparative terms a missile flying at subsonic speed can reach a maximum of 500 600 miles per hour To qualify as hypersonic a missile would have to move at least five times the speed of sound Mach The post Hypersonic missiles offer some impressive and disturbing capabilities appeared first on OxPol Between 2014 and June 2015 China conducted four major tests of its hypersonic missiles with a fifth test in August The fourth test of Wu 14 its ultra high speed nuclear delivery vehicle demonstrated a capacity for extreme maneuvers It was assessed as travelling at a speed of Mach 10 flying at 10 times the speed of sound or approximately 7 680 miles per hour To understand this in comparative terms a missile flying at subsonic speed can reach a maximum of 500 600 miles per hour To qualify as hypersonic a missile would have to move at least five times the speed of sound Mach The post Hypersonic missiles offer some impressive and disturbing capabilities appeared first on OxPol http://blog.politics.ox.ac.uk/11859-2/ http://blog.politics.ox.ac.uk/11859-2/ 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 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 The course begins with the basics of compressible fluid dynamics including governing equations thermodynamic context and characteristic parameters The next large block of lectures covers quasi one dimensional flow followed by a discussion of disturbances and unsteady flows The second half of the course comprises gas dynamic discontinuities including shock waves and detonations and concludes with another large block dealing with two dimensional flows both linear and non linear http://www.core.org.cn/OcwWeb/Aeronautics-and-Astronautics/16-120Spring2003/CourseHome/index.htm http://www.core.org.cn/OcwWeb/Aeronautics-and-Astronautics/16-120Spring2003/CourseHome/index.htm The course begins with the basics of compressible fluid dynamics including governing equations thermodynamic context and characteristic parameters The next large block of lectures covers quasi one dimensional flow followed by a discussion of disturbances and unsteady flows The second half of the course comprises gas dynamic discontinuities including shock waves and detonations and concludes with another large block dealing with two dimensional flows both linear and non linear https://ocw.mit.edu/courses/aeronautics-and-astronautics/16-120-compressible-flow-spring-2003 https://ocw.mit.edu/courses/aeronautics-and-astronautics/16-120-compressible-flow-spring-2003