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Publikováno v:
43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The left wing of the Active Aeroelastic Wing (AAW) F/A-18 airplane has been ground-load-tested to quantify its torsional stiffness. The test has been performed at the NASA Dryden Flight Research Center in November 1996, and again in April 2001 after
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47470989aabcb8fc4ae7e2c0bd54c23b
https://doi.org/10.2514/6.2002-1333
https://doi.org/10.2514/6.2002-1333
