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Subject Item: dbr:Bell_Boeing_Quad_TiltRotor
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Subject Item: dbr:Unitary_Plan_Wind_Tunnel_(Mountain_View,_California)
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Subject Item: dbr:Index_of_physics_articles_(S)
dbo:wikiPageWikiLink: dbr:Subsonic_and_transonic_wind_tunnel

Subject Item: dbr:Propulsion_Wind_Tunnel_Facility
dbo:wikiPageWikiLink: dbr:Subsonic_and_transonic_wind_tunnel

Subject Item: dbr:Notre_Dame_College_of_Engineering
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Subject Item: dbr:Subsonic
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Subject Item: dbr:Subsonic_and_transonic_wind_tunnel
rdfs:label: Subsonic and transonic wind tunnel
rdfs:comment: Low-speed wind tunnels are used for operations at very low Mach number, with speeds in the test section up to 480 km/h (~ 134 m/s, M = 0.4). They may be of open-return type (also known as the Eiffel type, see figure), or closed-return flow (also known as the Prandtl type, see figure) with air moved by a propulsion system usually consisting of large axial fans that increase the dynamic pressure to overcome the viscous losses.
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dcterms:subject: dbc:Wind_tunnels
dbo:wikiPageID: 3657610
dbo:wikiPageRevisionID: 1100183272
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dbo:abstract: Low-speed wind tunnels are used for operations at very low Mach number, with speeds in the test section up to 480 km/h (~ 134 m/s, M = 0.4). They may be of open-return type (also known as the Eiffel type, see figure), or closed-return flow (also known as the Prandtl type, see figure) with air moved by a propulsion system usually consisting of large axial fans that increase the dynamic pressure to overcome the viscous losses.
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Subject Item: dbr:Aircraft_industry_of_Serbia
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Subject Item: dbr:Focke's_wind_tunnel
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Subject Item: dbr:Aeronautical_Technical_Institute
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Subject Item: dbr:Campus_of_the_University_of_Notre_Dame
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