Aandacht voor veiligheid

Preliminary study of a plug nozzle model in supersonic flow

Experimental and computational study of a blunt cylinder-flare model in high supersonic flow

Surface flow visualization of a glancing shock-wave/ boundary-layer interaction

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

Hypersonic test facility Delft HTF-Delft

Investigation of the Vortex flow over a sharp-edged delta wing in the transonic speed regime

The calibration and measuring procedure of a five-hole hemispherical head probe in compressible flow

Experimental investigation of the transonic flow at the Leeward side of a delta wing at high incidence

A curved test section for research on transonic shock wave-boundary layer interaction

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

Numerical solution of transonic normal shock wave-boundary layer interaction using the Bohning-Zierep model

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

On the numerical computation of the supersonic flow field about blunted cones at small angles of incidence

Experimental investigation of the supersonic flow field about a slender cone at high incidences

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

An experimental investigation of the expansion flow field over a delta wing at supersonic speed

Enige visuele waarnemingen van de stroming in een twee-dimensionale inlaat met uitwendige compressie, ontworpen voor een getal van Mach van 2,94

Meting van de specifieke vochtigheid van de lucht in het voorraadvat van de ST15 supersone windtunnel