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Messrs Cooper, talking at motor car Messrs Cooper, talking at motor car

Description

Subjects

car | car | automobile | automobile | explore | explore | berkhamsted | berkhamsted | bessborough | bessborough | humber | humber | glassnegative | glassnegative | gaiters | gaiters | nationallibraryofireland | nationallibraryofireland | williamcooper | williamcooper | ahpoole | ahpoole | humberlimited | humberlimited | poolecollection | poolecollection | arthurhenripoole | arthurhenripoole | cooperssheepdip | cooperssheepdip | 1908humber | 1908humber | humber2seater | humber2seater | williamcoopernephews | williamcoopernephews

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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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Artesian Bore, East Moree

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Subjects

water | spout | powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27771

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Farm Cove from Macquarie Street

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27767

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The Domain

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Subjects

trees | harbour | sydney | domain | powerhousemuseum | the | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27766

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The Cliffs, Blue Lake, Kosciuszko

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Subjects

rocks | powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27762

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Stud Herefords

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Subjects

water | cows | hereford | willows | stud | powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27760

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On Rams Head Range, Kosciuszko

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Subjects

horses | mountains | grass | rest | powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27755

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A Stud Dairy Herd

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Subjects

cows | pasture | powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27754

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Bloody Bridge, Norfolk Island

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Subjects

powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27752

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Kuse's Bore

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27751

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Kuse's Bore

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27750

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No. 1 Bore, Cooncoola

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27749

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No. 3 Bore, Cooncoola

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27748

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Beels Bore

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27747

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Beels Bore

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27745

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Beels Bore

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27744

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Weelamurra Bore

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27742

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No. 1 Bore, Noorooma

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27741

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No. 1 Bore, Charlotte Plains, Q

Description

Subjects

powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27739

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No. 1 Bore, Charlotte Plains, Q

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powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27738

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No. 2 Bore, Charlotte Plains, Q

Description

Subjects

powerhousemuseum | xmlns:dc=httppurlorgdcelements11 | dc:identifier=httpwwwpowerhousemuseumcomcollectiondatabaseirn27737

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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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Thomas Smith

Description

Along with James Davit and William Cotter, Thomas Smith defrauded another gentlemen in 1873. Thomas was sentenced to carry out 3 months in Newcastle City Gaol. Age (on discharge): 32 Height: 5.5 Hair: Brown Eyes: Grey Place of Birth: New York Status: Widower Occupation: Shoemaker Reference:TWAS: PR.NC/6/1/1140 (Copyright) We're happy for you to share this digital image 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. To purchase a hi-res copy please email archives@twmuseums.org.uk quoting the title and reference number.

Subjects

thomassmith | jamesdavitwilliamcotterdefraudcriminalnewcastle | city | gaolhouse | correctioncrimeprevention | crimes | weartyne | wear | archives | museumsnorth | eastsepia | photosold | photographsnewcastletheftprison | 1871 | 1873 | prisoners | twam | tyne | socialhistory | sepiaphotograph | digitalimage | documentation | publicrecords | criminalrecord | criminalsof18711873 | 18711873 | portrait | historic | heritage | mugshot | accomplices | jamesdavit | williamcotter | defrauded | crime | offence | gentlemen | man | mascaline | male | sentenced | detained | conviction | 3monthsprisonterm | newcastlecitygaol | newcastleupontyne | northeastofengland | unitedkingdom | abstract | newyork | america | shoemaker | widower | chair | wood | seated | studio | room | interior | wall | neutralbackground | grain | mark | blur | beard | fixedeyes | attentive | blankexpression | coat | buttons | crease | trousers | pocket | unusual | fascinating

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Simcoe's Map of Williamsburg, Virginia

Description

Collection: A. D. White Architectural Photographs, Cornell University Library Accession Number: 15/5/3090.00554 Title: Simcoe's Map of Williamsburg, Virginia Mapmaker: Lt. Col. Simcoe Map date: ca. 1776-ca. 1782 Photograph date: ca. 1935 Location: North and Central America: United States; Virginia, Williamsburg Materials: gelatin silver print Image: 7 x 9 1/4 in.; 17.78 x 23.495 cm Provenance: Transfer from the College of Architecture, Art and Planning Persistent URI: hdl.handle.net/1813.001/5sp2 There are no known U.S. copyright restrictions on this image. The digital file is owned by the Cornell University Library which is making it freely available with the request that, when possible, the Library be credited as its source. We had some help with the geocoding from Web Services by Yahoo!

Subjects

cornelluniversitylibrary | maps | drawings | compasses | colonialwilliamsburgvirginia | culidentifier:value=155309000554 | culidentifier:lunafield=accessionnumber | simcoe | johngravessimcoe | williamsburg | virginia

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