Matches in DBpedia 2014 for { <http://dbpedia.org/resource/Supersonic_wind_tunnel> ?p ?o. }
Showing items 1 to 29 of
29
with 100 items per page.
- Supersonic_wind_tunnel abstract "A supersonic wind tunnel is a wind tunnel that produces supersonic speeds (1.2<M<5)The Mach number and flow are determined by the nozzle geometry. The Reynolds number is varied by changing the density level (pressure in the settling chamber). Therefore a high pressure ratio is required (for a supersonic regime at M=4, this ratio is of the order of 10). Apart from that, condensation of moisture or even gas liquefaction can occur if the static temperature becomes cold enough. This means that a supersonic wind tunnel usually needs a drying or a pre-heating facility.A supersonic wind tunnel has a large power demand, so that most are designed for intermittent instead of continuous operation.".
- Supersonic_wind_tunnel thumbnail Engineers_Check_Body_Revolution_Model_-_GPN-2000-001473.jpg?width=300.
- Supersonic_wind_tunnel wikiPageExternalLink watch?v=iNBZBChS2YI.
- Supersonic_wind_tunnel wikiPageID "3721032".
- Supersonic_wind_tunnel wikiPageRevisionID "597496973".
- Supersonic_wind_tunnel hasPhotoCollection Supersonic_wind_tunnel.
- Supersonic_wind_tunnel subject Category:Aerodynamics.
- Supersonic_wind_tunnel subject Category:Fluid_dynamics.
- Supersonic_wind_tunnel subject Category:Wind_tunnels.
- Supersonic_wind_tunnel type Artifact100021939.
- Supersonic_wind_tunnel type Object100002684.
- Supersonic_wind_tunnel type PhysicalEntity100001930.
- Supersonic_wind_tunnel type Structure104341686.
- Supersonic_wind_tunnel type Whole100003553.
- Supersonic_wind_tunnel type WindTunnel104591359.
- Supersonic_wind_tunnel type WindTunnels.
- Supersonic_wind_tunnel type YagoGeoEntity.
- Supersonic_wind_tunnel type YagoPermanentlyLocatedEntity.
- Supersonic_wind_tunnel comment "A supersonic wind tunnel is a wind tunnel that produces supersonic speeds (1.2<M<5)The Mach number and flow are determined by the nozzle geometry. The Reynolds number is varied by changing the density level (pressure in the settling chamber). Therefore a high pressure ratio is required (for a supersonic regime at M=4, this ratio is of the order of 10). Apart from that, condensation of moisture or even gas liquefaction can occur if the static temperature becomes cold enough.".
- Supersonic_wind_tunnel label "Supersonic wind tunnel".
- Supersonic_wind_tunnel label "Überschall-Windkanal".
- Supersonic_wind_tunnel sameAs Überschall-Windkanal.
- Supersonic_wind_tunnel sameAs m.09x5nt.
- Supersonic_wind_tunnel sameAs Q333195.
- Supersonic_wind_tunnel sameAs Q333195.
- Supersonic_wind_tunnel sameAs Supersonic_wind_tunnel.
- Supersonic_wind_tunnel wasDerivedFrom Supersonic_wind_tunnel?oldid=597496973.
- Supersonic_wind_tunnel depiction Engineers_Check_Body_Revolution_Model_-_GPN-2000-001473.jpg.
- Supersonic_wind_tunnel isPrimaryTopicOf Supersonic_wind_tunnel.