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- Hypersonic_wind_tunnel abstract "A hypersonic wind tunnel is designed to generate a hypersonic flow field in the working section, thus simulating the typical flow features of this flow regime - including compression shocks and pronounced boundary layer effects, entropy layer and viscous interaction zones and most importantly high total temperatures of the flow. The speed of these tunnels vary from Mach 5 to 15. The power requirement of a wind tunnel increases with the cross section, the flow density and is directly proportional to the third power of the test velocity. Hence installation of a continuous, closed circuit wind tunnel remains a costly affair. The first continuous Mach 7-10 wind tunnel with 1x1 m test section was planned at Kochel am See, Germany during WW II and finally put into operation as 'Tunnel A' in the late 1950s at AEDC Tullahoma, TN, USA for an installed power of 57 MW. In view of these high facility demands, also intermittently operated experimental facilities like blow-down wind tunnels are designed and installed to simulate the hypersonic flow. A hypersonic wind tunnel comprises in flow direction the main components: heater/cooler arrangements, dryer, convergent/divergent nozzle, test section, second throat and diffuser. A blow-down wind tunnel has a low vacuum reservoir at the back end, while a continuously operated, closed circuit wind tunnel has a high power compressor installation instead. Since the temperature drops with the expanding flow, the air inside the test section has the chance of becoming liquefied. For that reason, preheating is particularly critical (the nozzle may require cooling).".
- Hypersonic_wind_tunnel thumbnail Langley_hypersonic_wind_tunnels.jpg?width=300.
- Hypersonic_wind_tunnel wikiPageExternalLink 19640002194_1964002194.pdf.
- Hypersonic_wind_tunnel wikiPageExternalLink longshot.pdf.
- Hypersonic_wind_tunnel wikiPageID "3677421".
- Hypersonic_wind_tunnel wikiPageLength "4761".
- Hypersonic_wind_tunnel wikiPageOutDegree "23".
- Hypersonic_wind_tunnel wikiPageRevisionID "705221275".
- Hypersonic_wind_tunnel wikiPageWikiLink Arnold_Engineering_Development_Complex.
- Hypersonic_wind_tunnel wikiPageWikiLink Category:Aerodynamics.
- Hypersonic_wind_tunnel wikiPageWikiLink Category:Fluid_dynamics.
- Hypersonic_wind_tunnel wikiPageWikiLink Category:Wind_tunnels.
- Hypersonic_wind_tunnel wikiPageWikiLink Hypersonic_speed.
- Hypersonic_wind_tunnel wikiPageWikiLink Kelvin.
- Hypersonic_wind_tunnel wikiPageWikiLink Langley_Research_Center.
- Hypersonic_wind_tunnel wikiPageWikiLink Liquefaction.
- Hypersonic_wind_tunnel wikiPageWikiLink Ludwieg_tube.
- Hypersonic_wind_tunnel wikiPageWikiLink Mach_number.
- Hypersonic_wind_tunnel wikiPageWikiLink NASA.
- Hypersonic_wind_tunnel wikiPageWikiLink Pascal_(unit).
- Hypersonic_wind_tunnel wikiPageWikiLink Shock_tube.
- Hypersonic_wind_tunnel wikiPageWikiLink Subsonic_and_transonic_wind_tunnel.
- Hypersonic_wind_tunnel wikiPageWikiLink Supersonic_wind_tunnel.
- Hypersonic_wind_tunnel wikiPageWikiLink Von_Karman_Institute_for_Fluid_Dynamics_(VKI).
- Hypersonic_wind_tunnel wikiPageWikiLink Wind_tunnel.
- Hypersonic_wind_tunnel wikiPageWikiLink File:Langley_hypersonic_wind_tunnels.jpg.
- Hypersonic_wind_tunnel wikiPageWikiLink Talk:Hypersonic_wind_tunnel.
- Hypersonic_wind_tunnel wikiPageWikiLinkText "'Gun Tunnel'".
- Hypersonic_wind_tunnel wikiPageWikiLinkText "Gun Tunnel".
- Hypersonic_wind_tunnel wikiPageWikiLinkText "Hot shot wind tunnel, for hypersonic testing".
- Hypersonic_wind_tunnel wikiPageWikiLinkText "Hypersonic Tunnels".
- Hypersonic_wind_tunnel wikiPageWikiLinkText "Hypersonic wind tunnel".
- Hypersonic_wind_tunnel wikiPageWikiLinkText "hypersonic wind tunnel".
- Hypersonic_wind_tunnel wikiPageWikiLinkText "hypersonic".
- Hypersonic_wind_tunnel wikiPageUsesTemplate Template:Reflist.
- Hypersonic_wind_tunnel subject Category:Aerodynamics.
- Hypersonic_wind_tunnel subject Category:Fluid_dynamics.
- Hypersonic_wind_tunnel subject Category:Wind_tunnels.
- Hypersonic_wind_tunnel type Dynamic.
- Hypersonic_wind_tunnel type Mechanic.
- Hypersonic_wind_tunnel comment "A hypersonic wind tunnel is designed to generate a hypersonic flow field in the working section, thus simulating the typical flow features of this flow regime - including compression shocks and pronounced boundary layer effects, entropy layer and viscous interaction zones and most importantly high total temperatures of the flow. The speed of these tunnels vary from Mach 5 to 15.".
- Hypersonic_wind_tunnel label "Hypersonic wind tunnel".
- Hypersonic_wind_tunnel sameAs Q1641091.
- Hypersonic_wind_tunnel sameAs Hyperschall-Windkanal.
- Hypersonic_wind_tunnel sameAs m.09tyvt.
- Hypersonic_wind_tunnel sameAs Q1641091.
- Hypersonic_wind_tunnel wasDerivedFrom Hypersonic_wind_tunnel?oldid=705221275.
- Hypersonic_wind_tunnel depiction Langley_hypersonic_wind_tunnels.jpg.
- Hypersonic_wind_tunnel isPrimaryTopicOf Hypersonic_wind_tunnel.