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

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

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

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

Trailing-Edge Cavity Afterbodies for Linear Plug Nozzle Enginess

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

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

Experiments on a Linear Plug Nozzle with a VTEC Afterbody

CFD Validation for Base Flows with and without plume interaction

Trailing edge cavity afterbodies for linear plug nozzle engines

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

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

Half Model Restrictions for Linear Plug Nozzle Testing