Automotive Adsorption Air Conditioner Powered by Exhaust Heat. Part 2: Detailed Design and Analysis
Automotive Adsorption Air Conditioner Powered by Exhaust Heat. Part 2: Detailed Design and Analysis
Vulnerability of Spacecraft Electronics Boxes to Hypervelocity Impacts (IAC-05-B6.4.02)
A 3D model for eddy current inspection in aeronautics. Application to riveted structures
Improving the Significance of MM/SD Risk Analysis by Application of the SRL Ballistic Limit Equation
CFD Analysis of Radiative Heat Loading on Hypervelocity Re-Entry Vehicles
North East Aircraft Museum : New England Air Museum, Aviation, RAF Usworth
CFD Modelling of Re-Entry Flows Including Gas Radiation
Simulation of a Mars Aerocapture Vehicle on Flow Adapted Unstructured Grids with the DLR TAU Code