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Article | REF: TRP4015 V1

Aeronautical Wind Tunnels. Achitecture, Testing Process, Measurements Techniques

Authors: Sylvain MOUTON, François GARÇON

Publication date: July 10, 2022 | Lire en français

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    2. Wind tunnel architecture

    2.1 Subsonic and transsonic wind tunnels

    These are the most frequently encountered installations, since they correspond to the flight envelope of a large proportion of aircraft, and in particular all civil aircraft. Although they cover different flight envelopes, their architecture is largely similar, as shown in figure 4 .

    Subsonic wind tunnels cover the Mach number range from 0 to around 0.6, for which gas compressibility effects remain moderate (see figure 2 ). Transonic wind tunnels...

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