Wind Tunnel Description
Aerodynamic Configuration
Aero-Acoustic Configuration
Instrumentation
Special Features and Equipment
Equipment Loan Form
Publications Listing
Pictures from Research Projects
The Virginia Tech Six Foot Stability Wind Tunnel was originally built at the NACA Langley Aeronautical Laboratory in 1940. It was designed to determine dynamic stability derivatives using a fixed model position, and was known at Langley as the "stability tunnel." Many of the NACA reports containing stability derivative data describe wind tunnel tests conducted in this tunnel. The wind tunnel was acquired by VPI in 1958, and the tunnel was erected in 1959 in a specially designed wing of Randolph Hall. Calibration of the tunnel was carried out from 1959 to 1961, when it became operational again. In 1994 the fan motor was completely overhauled and the windings reinsulated. In 1996 new fan blades were installed increasing the overall tunnel efficiency. Figures 1 and 2 show the tunnel as it exists today at the university. The new fan blades are shown in Figure 3.
Figure 1: Virginia Tech 6' x 6' Stability Tunnel showing drive section and air exchange tower.
Figure 2: Stability tunnel showing connection to Randolph Hall through metal building at center of picture. This pressure sealed building contains both the test section and operating console, such that the operators work at the test section static pressure level.
Figure 3: Stability tunnel fan with new fan blades custom manufactured by Prince Aircraft Company (1996).
For prospective customers interested in the facility please consult the schedule and e-mail your requests as follows: