Compressibility effects for the AGARD-B model
(2015)
Journal Article
A numerical study of the flow topologies over the 60° delta wing of the AGARD-B model at Mach 0 · 80 has revealed that vortex bursting occurs between 13°-15° angle-of-attack, while vortex separation occurs above 18°. These aerodynamic features have b... Read More about Compressibility effects for the AGARD-B model.