Aerodynamic Load Analysis of a Variable Camber Continuous Trailing Edge Flap System on a Flexible Wing Aircraft (AIAA 2015-1839)
AIAA/ASME/ASME/ASCE/AHS/SC Structures, structural dynamics and materials (Conference)
2015-01-01
47 pages
Aufsatz (Konferenz)
Englisch
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British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2015
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