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HUBSCHRAUBER
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keywords:(HUBSCHRAUBER)
Five helicopter accidents with evidence of material and/or design deficiencies
Civil and military design requirements and their influence on the product
Strukturveraenderung in der italienischen Hubschrauberindustrie
Adaptation of pultrusion to the manufacture of helicopter components
Survey of fatigue failures in helicopter components and some lessons learnt
An easy way to model helicopter flight
Helicopter reliability and maintainability trends during development and production
Combined military and commercial application of light helicopters
Effects of flight load spectrum perturbations on cost and fatigue
Determining the contour of helicopter rotor blades automatically using electro-optical techniques
Innovations in epicyclic gear system design for increased service life
Research requirements for the improvement of helicopter operations
Salons internationaux de l'aeronautique et de l'espace. Un salon de plus en plus international
Identification of abnormal events by data monitoring: Application to complex systems
Model of multidisciplinary simulation integration in helicopter rotor blade design process
Reliability improvement warranty (RIW) and the army lightweight doppler navigation system (LDNS)
Association technique maritime et aeronautique (A.T.M.A.)
Evaluation of dry lubricated aircraft control cables and pulley wheels
Life cycle cost as a propulsion system design consideration
Engine/airframe/drive train dynamic interface documentation
Single-Engine piston helicopters, Singel-engine turbine helicopters, multiengine turbine helicopters
Multicyclic jet-flap control for alleviation of helicopter blade stresses and fuselage vibration
Ferrography as a health monitor and a design aid for the development ofhelicopter gearboxes
Soft computing feature extraction for health monitoring of rotorcraft structures
Soft computing signal processing for health monitoring of tie-bar of rotor head structure
Technical and operational aspects of helicopter civil service
Liquid composite molding for aeronautical structures