bn:03040129n
Noun Concept
EL
υπερυπερηχητικών αεροδυναμική σήραγγα
EN
A hypersonic wind tunnel is designed to generate a hypersonic flow field in the working section, thus simulating the typical flow features of this flow regime - including compression shocks and pronounced boundary layer effects, entropy layer and viscous interaction zones and most importantly high total temperatures of the flow. Wikipedia
Relations
Sources