Airplane wing load control systems are designed for modification/redistribution of aerodynamic loads in order to decrease risk of structural damage in conditions of excessive loads, to improve passenger comfort in turbul...
EP ID EP65197
DOI -
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How To Cite
Krzysztof Dudzik (2013). INFLUENCE OF JOINING METHOD FOR MECHANICAL PROPERTIES OF 7020 ALUMINIUM ALLOY JOINTS. Journal of KONES, 20(1),
71-76. https://europub.co.uk/articles/-A-65197
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NUMERICAL MODEL OF FRICIONAL DAMPER FOR GLAS-MAKING ROBOT LANCE
HEADLIGHTS TYPE APPROVAL REQUIREMENTS AND ON FIELD REQUIREMENTS - TECHNICAL IMPACT ON SAFETY
EXPERIMENTAL INVESTIGATION OF IED INTERROGATION ARM DURING NORMAL OPERATION
RESEARCH OF WATER-FUEL MICROEMULSIONS AS FUEL FOR DIESEL ENGINE
MODIFICATION OF AERODYNAMIC WING LOADS BY FLUIDIC DEVICES
Airplane wing load control systems are designed for modification/redistribution of aerodynamic loads in order to decrease risk of structural damage in conditions of excessive loads, to improve passenger comfort in turbul...