Numerical Simulation of a Complete Low-Speed Wind Tunnel Circuit

A numerical simulation of the complete circuit of the NASA Langley 14 x 22-ft low-speed wind tunnel is described. Inside the circuit, all turning vanes are modeled as well as the five flow control vanes downstream of the 1st corner. The fan drive system is modeled using an actuator disk for the fan...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Nayani, Sudheer N., Sellers, William L., III, Tinetti, Ana F., Brynildsen, Scott E., Walker, Eric L.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerodynamics Numerical Analysis
Online-Zugang:	Volltext bestellen
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