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:Vallabh, Bhavya; Skews, BWDate:Sep 2017The existing nozzle contour profiles of the CSIR’s supersonic or High Speed Wind Tunnel (HSWT) produce weak waves in the test section region, which effectively degrades the air flow quality in the test section. This paper describes a calculation ...Read more