Flow visualization study of high supersonic flow past a blunt cylinder-cone flare body

Hypersonic test facility Delft HTF-Delft

Transonic Mach number determination in a blow-down windtunnel with solid walls and a downstream throat

In this report calibration measurements are described of the transonic flow in the TST27 windtunnel (test section: 28 cm x 25.3 cm) of the Laboratory for High Speed Aerodynamics, Department of Aerospace Engineering, University of Technology Delft. The tunnel has solid walls and the Mach number in the high subsonic and transonic flow regime is...

Transonic Mach number determination in a blow-down wind-tunnel with solid walls and a downstream throat

On the structure of the potential flow field near conical stagnation points in supersonic flow

Bepaling van het getal van Mach van de transsone stroming in de TST 27 windtunnel met dichte wanden

Conical stagnation points in the supersonic flow around slender circular cones at incidence