Synonyme wurden verwendet für:
Flugzeug
•
Tragwerk
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keywords:(Tragwerk (Flugzeug))
Structural Optimization of Box Wing Aircraft
Risikobasierte Überwachungsverfahren zur Lebensdauerverlängerung von bestehenden und neuen Bauwerken
Marker loads for quantitative fractography of fatigue cracks in aerospace alloys
Time-variant aerodynamics for torsional motion of large-turning airfoils
LPV-model based identification approach of oscillatory failure cases
Multiple crack considerations for skin joints in high life aircraft
A growth model for catastrophic cracking in an RAAF aircraft
Uncertainty quantification of structural response using evidence theory
Structures technology of modern general aviation aircraft
Friction stir welding industrial applications worldwide
Optimale Leitwerkauslegung fuer Flugzeuge kuenstlicher Stabilitaet
Im MRCA-Programm beginnt die Fertigungsinvestitionsphase
A bio-inspired study on tidal energy extraction with flexible flapping wings
Friction welding and laser heat treatment of dissimilar metals
Part-through crack problems in aircraft structures
Dynamics and Control of a Flexible Flapping Wing Aircraft
Aeroelastic Behavior of Morphing Wing in Flutter Regions
Some practical aspects of viscous drag reduction concepts
Appraoximationspolynome der Methode der Finiten Elemente des Lagrangeschen Variationsprinzip
Aeroelastic properties of straight and forward swept graphite/epoxy wings
Präzision ist Trumpf. Automatisierung im Flugzeugbau
Corrosion fatigue through particle swarm optimization
Response surface approximations: Noise, error repair, and modeling errors
Manufacturability-based optimization of aircraft structures using physical programming
Supercritical wing design using numerical optimization and comparison with experiment
Design development of unitized titanium structure
Betriebsfestigkeitsnachweis für das Teleskop-Lager beim Projekt SOFIA
Multiple hollow sphere core sandwich fabrication
Integrale Fluegel/Rumpf-Struktur aus CFK bei Kampfflugzeugen
Wing-tail interaction flutter revisited
Untersuchung der Festigkeit einer Flugzeugkonstruktion mit Hilfe eines mathematischen Modells
Use of substructural transmission zeros for structural health monitoring
Increasing allowable flight loads by improved structural modeling
Application of advanced materials: Weight saving potential in future transport aircraft
Existence and uniqueness of shock-free transonic flow past symmetrical thin wings at zero incidence
Laserstrahlbiegen komplexer Aluminiumstrukturen für Anwendungen in der Luftfahrtindustrie
Probabilistic analysis of multi-site damage in aircraft fuselages
Effects of age and use on Apache main rotor support characteristics
Aeroelastic tailoring of advanced composite lifting surfaces in preliminary design
Evaluation of damage tolerance analysis tools for lap joints
Aeroelastic tailoring of composite materials to improve performance
Integriertes Fluegel-Antriebs-System (IFAS) - Phase II