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Fluid mechanics / Wind tunnels / Airspeed / Mach number / Scramjet / Hypersonic speed / Supersonic wind tunnel / Computational fluid dynamics / Hypersonic wind tunnel / Aerodynamics / Aerospace engineering / Fluid dynamics


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Document Date: 2007-09-17 12:14:02

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File Size: 826,17 KB

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City

Novosibirsk / /

Company

AeroSoft Inc. / John Wiley & Son Inc / /

Country

Russia / /

Currency

pence / /

Facility

Virginia Tech Hypersonic Wind Tunnel / Institute of Theoretical / /

IndustryTerm

steady-state solutions / time-accurate solution / steady-state flowfield solution / time-accurate solutions / flowfield solutions / numerical solutions / Implicit dual time stepping algorithm / internal energy / /

NaturalFeature

Nozzle Inlet / /

Organization

Institute of Theoretical and Applied Mechanics / VIRGINIA TECH HYPERSONIC WIND TUNNEL Rui Chen Department of Aerospace & Ocean Engineering / Institute of Theoretical / Virginia Tech / Applied Mechanics / /

Person

Van Albada / Reece Neel / Joseph Schetz / /

Position

advisor / General / /

Technology

Implicit dual time stepping algorithm / fluid dynamics / ATM / Simulation / 8 processors / obtained using a computational fluid dynamics / /

URL

http /

SocialTag