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Flugzeugbau
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6H-SiC transistor integrated circuits demonstrating prolonged operation at 500 deg C
400Hz generators evolution, effects of installation arrangements
ABiTAS. Advanced Bonding Technologies for Aircraft Structures
A brushless DC permanent magnet motor - the basis of electric drives for all-electric aircraft
Accuracy of a simple hole damage analysis method in composite structures
A chromate-free post-anodising treatment for aluminium alloys using a double-immersion process
A close-coupled canard, technology demonstration aircraft for general aviation applications
A concept for reduction of structure activitation with robust control
Acoustic measurements in a small transmission loss facility
A design scheme aimed at minimizing actuator and structural loads of a span morphing aircraft
Adhesion and flexibility of pretreatments and primers for aircraft
Adhesive bonded structure of new pressurized piston twin aircraft
Advanced analysis tools for concurrent/integrated engineering of composite airframe structures
Advanced gearboxes for a modern single rotation turboprop engine
Advanced knowledge system for coatings and the gas turbine MRO industry
Advanced liquid-cooled, turbo-charged and intercooled stratified charge rotary engines for aircraft
Aerodynamic development of a high pressure leading edge blowing boundary layer control system
Aerodynamic modelling for flight dynamics analysis of conceptual aircraft designs
Aerodynamic optimization and analysis as part of the computer-aided design process
Aerodynamic performance of acoustically suppressed exhaust nozzles
Aerodynamic-performance planform and camber optimization of a supersonic transport wing
Aerodynamic wing optimisation using SOMA evolutionary algorithm
Aerospace corrosion control symposium - corrosion behind the sheets
Aerospace manufacturing techniques for thermoplastic composites
A fracture mechanics study of the residual strength of pin-lug specimens
A generalized mathematical model to estimate gas turbine starting characteristics
A hybrid subspace analysis procedure for non-linear postbuckling calculation