Description and Flow Assesment of the Delft Hypersonic Ludwieg Tube

Investigation of a sharp-edged delta wing in a supersonic flow using stereo PIV

Proposal for a research activity competing in the European Space Agency

Application of PIV in a hypersonic double-ramp flow. Paper AIAA-2005-3331

Experiments on hypersonic roughness induced transition by means of infrared thermography. Paper no: 9443

Analytical Optimisation of an Inviscid Flow Linear Plug Nozzle Boattail. AIAA-2004-4017

Experimental investigation of supersonic base flow plume interaction by means of Particle Image Velocimetry

TVC and Side Fence Calculations on the LION Plug Nozzle (AIAA-2003-7003)

Trailing-Edge Cavity Afterbodies for Linear Plug Nozzle Enginess

Feasibility study of an (optical) diagnostic techniques in the development of the hot-plume testing facility

CFD Validation for Base Flows with and without plume interaction

Experiments on a Linear Plug Nozzle with a VTEC Afterbody

Experimental Investigation of Base Pressure with Hot Supersonic Jet for External Supersonic Flow

Trailing edge cavity afterbodies for linear plug nozzle engines

Half Model Restrictions for Linear Plug Nozzle Testing

Computational Study of Support Influence on Base Flow of a Model in Supersonic Flow