Effect of boundary layers on solid walls in three-dimensional subsonic wind tunnels

Adcock, J. B.; Barnwell, R. W.

doi:10.2514/6.1983-144

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1997

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“…This latter approximation is only valid for Mach numbers close to unity. Then, combining the approximate form of Equation (4) with Equations (5), (6) and (8), they obtained…”

Section: DX Dxmentioning

confidence: 99%

Recent experience in the prediction and assessment of windtunnel wall interference

Ashill¹,

Jordan²,

Simmons³

1997

Aeronaut. j.

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Recent experience in the prediction and assessment of windtunnel wall interference is reviewed. Three areas of development are identified. The first deals with the influence of wall boundary layers on wall-induced velocities in solid-wall windtunnels; the second is concerned with preparations for determining wall interference in the European Transonic Windtunnel and the third relates to recent studies aimed at providing the basis for correcting data to free-air conditions.

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“…This latter approximation is only valid for Mach numbers close to unity. Then, combining the approximate form of Equation (4) with Equations (5), (6) and (8), they obtained…”

Section: DX Dxmentioning

confidence: 99%