NASA NTRS · 19750034270
Development of minimum correction wind tunnels
Abstract
Flow distortions due to wind tunnel wall interference may be accounted for if the model to tunnel ratio is small, but the theory becomes less reliable as the model becomes larger. This paper presents theoretical analysis and experimental evidence which supports a new concept of wind tunnel. The method employs active control of flow through the walls so that the model is in approximately free air conditions during the test. Practical considerations in the design of such a tunnel are presented. Results indicate that a minimum correction wind tunnel may be achieved with active walls of relatively low porosity.
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Bernstein, S., Joppa, R. G.. 1975-01-01. Development of minimum correction wind tunnels. https://ntrs.nasa.gov/citations/19750034270
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