Author:Tuling, S; Vallabh, Bhavya; Morelli, Mauro FDate:Apr 2015A 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 ...Read more
Author:Tuling, S; Dala, L; Toomer, CDate:Dec 2013A numerical and experimental investigation was performed to study the dominant flow structures in the lee side of a cruciform wing–body configuration at supersonic speeds in the + orientation. The wings or strakes are of very low aspect ratio ...Read more