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16.100 Aerodynamics (MIT) 16.100 Aerodynamics (MIT)

Description

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. Technical RequirementsFile decompression software, such as Winzip® or StuffIt®, is required to open the .tar files found on this course site. 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. Technical RequirementsFile decompression software, such as Winzip® or StuffIt®, is required to open the .tar files found on this course site. MATLAB&#1

Subjects

aerodynamics | aerodynamics | airflow | airflow | air | air | body | body | aircraft | aircraft | aerodynamic modes | aerodynamic modes | aero | aero | forces | forces | flow | flow | computational | computational | CFD | CFD | aerodynamic analysis | aerodynamic analysis | lift | lift | drag | drag | potential flows | potential flows | imcompressible | imcompressible | supersonic | supersonic | subsonic | subsonic | panel method | panel method | vortex lattice method | vortex lattice method | boudary layer | boudary layer | transition | transition | turbulence | turbulence | inviscid | inviscid | viscous | viscous | euler | euler | navier-stokes | navier-stokes | wind tunnel | wind tunnel | flow similarity | flow similarity | non-dimensional | non-dimensional | mach number | mach number | reynolds number | reynolds number | integral momentum | integral momentum | airfoil | airfoil | wing | wing | stall | stall | friction drag | friction drag | induced drag | induced drag | wave drag | wave drag | pressure drag | pressure drag | fluid element | fluid element | shear strain | shear strain | normal strain | normal strain | vorticity | vorticity | divergence | divergence | substantial derviative | substantial derviative | laminar | laminar | displacement thickness | displacement thickness | momentum thickness | momentum thickness | skin friction | skin friction | separation | separation | velocity profile | velocity profile | 2-d panel | 2-d panel | 3-d vortex | 3-d vortex | thin airfoil | thin airfoil | lifting line | lifting line | aspect ratio | aspect ratio | twist | twist | camber | camber | wing loading | wing loading | roll moments | roll moments | finite volume approximation | finite volume approximation | shocks | shocks | expansion fans | expansion fans | shock-expansion theory | shock-expansion theory | transonic | transonic | critical mach number | critical mach number | wing sweep | wing sweep | Kutta condition | Kutta condition | team project | team project | blended-wing-body | blended-wing-body | computational fluid dynamics | computational fluid dynamics | Incompressible | Incompressible

License

Content within individual OCW courses is (c) by the individual authors unless otherwise noted. MIT OpenCourseWare materials are licensed by the Massachusetts Institute of Technology under a Creative Commons License (Attribution-NonCommercial-ShareAlike). For further information see http://ocw.mit.edu/terms/index.htm

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Sheriff on his horse at the Hoppings Sheriff on his horse at the Hoppings

Description

Subjects

1920s | 1920s | boy | boy | horse | horse | woman | woman | man | man | blur | blur | industry | industry | stockings | stockings | hat | hat | shirt | shirt | standing | standing | scarf | scarf | 1932 | 1932 | outdoors | outdoors | shoe | shoe | lights | lights | glasses | glasses | necklace | necklace | interesting | interesting | shine | shine | hand | hand | lordmayor | lordmayor | dress | dress | unitedkingdom | unitedkingdom | debris | debris | grain | grain | decoration | decoration | hats | hats | tie | tie | bowtie | bowtie | twist | twist | carousel | carousel | pole | pole | suit | suit | nostril | nostril | cap | cap | archives | archives | wife | wife | leisure | leisure | ribbon | ribbon | unusual | unusual | sheriff | sheriff | 1912 | 1912 | seated | seated | funfair | funfair | tyneside | tyneside | attentive | attentive | waistcoat | waistcoat | distracted | distracted | newcastleupontyne | newcastleupontyne | fascinating | fascinating | 1877 | 1877 | digitalimage | digitalimage | blyth | blyth | citycouncil | citycouncil | alderman | alderman | townmoor | townmoor | amusementride | amusementride | socialhistory | socialhistory | hoppings | hoppings | northeastengland | northeastengland | blackandwhitephotograph | blackandwhitephotograph | gallopinghorses | gallopinghorses | northeastofengland | northeastofengland | royalvictoriainfirmary | royalvictoriainfirmary | 192425 | 192425 | servingthecity | servingthecity | 193637 | 193637 | fundraisingday | fundraisingday | johngrantham | johngrantham | temperancefestival | temperancefestival | 26june1925 | 26june1925 | sheriffofnewcastle | sheriffofnewcastle | townmoortemperancefestivalhoppings | townmoortemperancefestivalhoppings | mrsgrantham | mrsgrantham

License

No known copyright restrictions

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16.100 Aerodynamics (MIT) 16.100 Aerodynamics (MIT)

Description

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.

Subjects

aerodynamics | aerodynamics | airflow | airflow | air | air | body | body | aircraft | aircraft | aerodynamic modes | aerodynamic modes | aero | aero | forces | forces | flow | flow | computational | computational | CFD | CFD | aerodynamic analysis | aerodynamic analysis | lift | lift | drag | drag | potential flows | potential flows | imcompressible | imcompressible | supersonic | supersonic | subsonic | subsonic | panel method | panel method | vortex lattice method | vortex lattice method | boudary layer | boudary layer | transition | transition | turbulence | turbulence | inviscid | inviscid | viscous | viscous | euler | euler | navier-stokes | navier-stokes | wind tunnel | wind tunnel | flow similarity | flow similarity | non-dimensional | non-dimensional | mach number | mach number | reynolds number | reynolds number | integral momentum | integral momentum | airfoil | airfoil | wing | wing | stall | stall | friction drag | friction drag | induced drag | induced drag | wave drag | wave drag | pressure drag | pressure drag | fluid element | fluid element | shear strain | shear strain | normal strain | normal strain | vorticity | vorticity | divergence | divergence | substantial derivative | substantial derivative | laminar | laminar | displacement thickness | displacement thickness | momentum thickness | momentum thickness | skin friction | skin friction | separation | separation | velocity profile | velocity profile | 2-d panel | 2-d panel | 3-d vortex | 3-d vortex | thin airfoil | thin airfoil | lifting line | lifting line | aspect ratio | aspect ratio | twist | twist | camber | camber | wing loading | wing loading | roll moments | roll moments | finite volume approximation | finite volume approximation | shocks | shocks | expansion fans | expansion fans | shock-expansion theory | shock-expansion theory | transonic | transonic | critical mach number | critical mach number | wing sweep | wing sweep | Kutta condition | Kutta condition | team project | team project | blended-wing-body | blended-wing-body | computational fluid dynamics | computational fluid dynamics

License

Content within individual OCW courses is (c) by the individual authors unless otherwise noted. MIT OpenCourseWare materials are licensed by the Massachusetts Institute of Technology under a Creative Commons License (Attribution-NonCommercial-ShareAlike). For further information see http://ocw.mit.edu/terms/index.htm

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Edexcel HND unit : engineering science (Nqf L4) : document transcript

Description

This open educational resource was released through the Higher Education Academy Engineering Subject Centre Open Engineering Resources Pilot project. The project was funded by HEFCE and the JISC/HE Academy UKOER programme.

Subjects

ukoer | engscoer | cc-by | leicester college | leicester college tech | leicestercollegeoer | engineering department | education | higher education | learning | stress | potential | columns | strain | linear motion | angular motion | statics | engineering science | beams | nqfl4 | kinetic | edexcel hnd unit | bending moment | rotation | stiffness | slenderness ratio | young's modulus | torsion | hnd | 2009-2010 | twisting | energy | shear force | edexcel hn unit engineering science | struts | Engineering | H000

License

Attribution 2.0 UK: England & Wales Attribution 2.0 UK: England & Wales http://creativecommons.org/licenses/by/2.0/uk/ http://creativecommons.org/licenses/by/2.0/uk/

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Introduction to torsion : document transcript

Description

This open educational resource was released through the Higher Education Academy Engineering Subject Centre Open Engineering Resources Pilot project. The project was funded by HEFCE and the JISC/HE Academy UKOER programme.

Subjects

ukoer | engscoer | cc-by | leicester college | leicester college tech | leicestercollegeoer | engineering department | education | higher education | learning | nqf l4 | engineering science | torsional stiffness | torsion | twisting | edexcel hn unit | edexcel | torsional | science | introduction to torsion | torque | engineering | stiffness | shaft | power | Engineering | H000

License

Attribution 2.0 UK: England & Wales Attribution 2.0 UK: England & Wales http://creativecommons.org/licenses/by/2.0/uk/ http://creativecommons.org/licenses/by/2.0/uk/

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Sheriff on his horse at the Hoppings

Description

View of John Grantham, Sheriff of Newcastle at the Town Moor Temperance Festival (Hoppings), 26 June 1925 (TWAM ref. DF.GRA/1/3). He and Mrs Grantham were involved with a special fundraising day at the Festival in support of the Royal Victoria Infirmary. These images belong to a series of albums documenting John Grantham?s service to the City of Newcastle upon Tyne as its Sheriff 1924-1925 and its Lord Mayor 1936-1937. John Grantham was born in Blyth in 1877 and became a cinema proprietor in Newcastle. He was elected to the City Council in 1912 and became an alderman in 1932. The albums give us an interesting insight into the duties of Lord Mayor and Sheriff as well as a fascinating picture of the times. 2016 is the 800th anniversary of the creation of Newcastle's Mayoralty and Burgesses. (Copyright) We're happy for you to share these digital images within the spirit of The Commons. Please cite 'Tyne & Wear Archives & Museums' when reusing. Certain restrictions on high quality reproductions and commercial use of the original physical version apply though; if you're unsure please email archives@twmuseums.org.uk

Subjects

johngrantham | sheriff | newcastleupontyne | townmoor | temperancefestival | hoppings | funfair | 1920s | hats | northeastengland | tyneside | carousel | gallopinghorses | socialhistory | blackandwhitephotograph | amusementride | digitalimage | industry | archives | northeastofengland | unitedkingdom | servingthecity | outdoors | blur | grain | pole | twist | horse | woman | scarf | dress | hat | man | cap | glasses | tie | shirt | suit | waistcoat | necklace | decoration | lights | ribbon | boy | bowtie | stockings | shoe | shine | fascinating | interesting | unusual | sheriffofnewcastle | townmoortemperancefestivalhoppings | 26june1925 | wife | mrsgrantham | fundraisingday | royalvictoriainfirmary | 192425 | lordmayor | 193637 | blyth | 1877 | citycouncil | 1912 | alderman | 1932 | leisure | attentive | distracted | seated | standing | hand | nostril | debris

License

No known copyright restrictions

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Tyne & Wear Archives & Museums | FlickR

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X0002P0215

Description

Corkscrew claw which did not cause lameness

Subjects

svmsvet | cow | bovine | foot | hoof | claw | corkscrew | twisted | horn

License

http://creativecommons.org/licenses/by-nc-sa/2.0/

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Nottingham Vet School | FlickR

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X0002P0215

Description

Corkscrew claw which did not cause lameness

Subjects

svmsvet | cow | bovine | foot | hoof | claw | corkscrew | twisted | horn

License

http://creativecommons.org/licenses/by-nc-sa/2.0/

Site sourced from

Nottingham Vet School | FlickR

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16.100 Aerodynamics (MIT)

Description

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.

Subjects

aerodynamics | airflow | air | body | aircraft | aerodynamic modes | aero | forces | flow | computational | CFD | aerodynamic analysis | lift | drag | potential flows | imcompressible | supersonic | subsonic | panel method | vortex lattice method | boudary layer | transition | turbulence | inviscid | viscous | euler | navier-stokes | wind tunnel | flow similarity | non-dimensional | mach number | reynolds number | integral momentum | airfoil | wing | stall | friction drag | induced drag | wave drag | pressure drag | fluid element | shear strain | normal strain | vorticity | divergence | substantial derivative | laminar | displacement thickness | momentum thickness | skin friction | separation | velocity profile | 2-d panel | 3-d vortex | thin airfoil | lifting line | aspect ratio | twist | camber | wing loading | roll moments | finite volume approximation | shocks | expansion fans | shock-expansion theory | transonic | critical mach number | wing sweep | Kutta condition | team project | blended-wing-body | computational fluid dynamics

License

Content within individual OCW courses is (c) by the individual authors unless otherwise noted. MIT OpenCourseWare materials are licensed by the Massachusetts Institute of Technology under a Creative Commons License (Attribution-NonCommercial-ShareAlike). For further information see https://ocw.mit.edu/terms/index.htm

Site sourced from

https://ocw.mit.edu/rss/all/mit-allcourses.xml

Attribution

Click to get HTML | Click to get attribution | Click to get URL

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16.100 Aerodynamics (MIT)

Description

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. Technical RequirementsFile decompression software, such as Winzip® or StuffIt®, is required to open the .tar files found on this course site. MATLAB&#1

Subjects

aerodynamics | airflow | air | body | aircraft | aerodynamic modes | aero | forces | flow | computational | CFD | aerodynamic analysis | lift | drag | potential flows | imcompressible | supersonic | subsonic | panel method | vortex lattice method | boudary layer | transition | turbulence | inviscid | viscous | euler | navier-stokes | wind tunnel | flow similarity | non-dimensional | mach number | reynolds number | integral momentum | airfoil | wing | stall | friction drag | induced drag | wave drag | pressure drag | fluid element | shear strain | normal strain | vorticity | divergence | substantial derviative | laminar | displacement thickness | momentum thickness | skin friction | separation | velocity profile | 2-d panel | 3-d vortex | thin airfoil | lifting line | aspect ratio | twist | camber | wing loading | roll moments | finite volume approximation | shocks | expansion fans | shock-expansion theory | transonic | critical mach number | wing sweep | Kutta condition | team project | blended-wing-body | computational fluid dynamics | Incompressible

License

Content within individual OCW courses is (c) by the individual authors unless otherwise noted. MIT OpenCourseWare materials are licensed by the Massachusetts Institute of Technology under a Creative Commons License (Attribution-NonCommercial-ShareAlike). For further information see https://ocw.mit.edu/terms/index.htm

Site sourced from

https://ocw.mit.edu/rss/all/mit-allarchivedcourses.xml

Attribution

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