3. Test process
3.1 Aircraft models and supports
The choice of scale is essentially dictated by the size of the wind tunnel. Some models are designed to be tested in several wind tunnels, in which case the scale is determined by the most stringent.
For Mach numbers below 1, the effect of the walls should not be too great, and the associated correction (see §
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Test process
Bibliography
Standards and norms
- Flight mechanics – concepts, quantities and symbols. - ISO 1151 - 1988
- Mesure de débit des fluides au moyen d'appareils déprimogènes insérés dans des conduites en charge de section circulaire (parties 1 à 4). - ISO 5167 - (2003)
Websites
Office national d'études et de recherches aérospatiales (ONERA - French national aerospace research agency)
German-Dutch Wind Tunnels
European Transonic Wind Tunnel ETW
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