Supersonic plasma jets device for testing spacecraft materials
Computation of non-winged vehicle aerodynamics in the low supersonic range
Major lessons learned in hypersonic design of Hermes
CFD-based design of the elevons of the Hermes spacecraft
Experimental and numerical analysis of a blunt body configuration in T5 and HEG
Aerodynamic off-design behaviour of integrated waveriders from take-off up to hypersonic flight
Reentry simulation within an induction heated plasma wind tunnel
Uncertainties in the numerical prediction of hypersonic flows
Experiment and computation of kinetic heating for two basic test flows
The structure of the relaxation zone behind shock waves in the reacting gas flows
Progress in low enthalpy hypersonic wind tunnel testing
A hypersonic flowfield around a reentry body including detailed base flow
Aerothermodynamic data base from high enthalpy facilities