The Modular Test Stand was developed and manufactured to decrease the cost of fatigue testing and reduce the time of its completion as well as to enable testing specimens under more complex load conditions. The stand consists of three connected sections, similar to a wing box, all being loaded in the same way. Thanks to that, several specimens can be tested simultaneously. This configuration requires that stress and strain distribution should be reasonably uniform, as assumed in the design stage. The structure can be loaded with bending or torsion. A whole section, selected structural node or a specimen mounted in the structure as well as a repair or a sensor can be a test object.
Modular Test Stand for Fatigue Testing of Aeronautical Structures – Verification of Assumptions
2020
Aufsatz (Zeitschrift)
Elektronische Ressource
Unbekannt
fatigue , test , airframe , veryfication , strain gauge , dic , Transportation engineering , TA1001-1280
Metadata by DOAJ is licensed under CC BY-SA 1.0
Conception of Modular Test Stand for Fatigue Testing of Aeronautical Structures
Springer Verlag | 2019
|Design of an Aeronautical Engine Test Stand
SAE Technical Papers | 2000
|PRACTICAL FATIGUE LOADINGS FOR AERONAUTICAL STRUCTURES
AIAA | 1964
|