The NASA Langley Aeroelasticity Branch is involved in a number of research programs related to fixed wing aeroelasticity and aeroservoelasticity. These ongoing efforts are summarized here, and include aeroelastic tailoring of subsonic transport wing structures, experimental and numerical assessment of truss-braced wing flutter and limit cycle oscillations, and numerical modeling of high speed civil transport configurations. Efforts devoted to verification, validation, and uncertainty quantification of aeroelastic physics in a workshop setting are also discussed. The feasibility of certain future civil transport configurations will depend on the ability to understand and control complex aeroelastic phenomena, a goal that the Aeroelasticity Branch is well-positioned to contribute through these programs.
Ongoing Fixed Wing Research within the NASA Langley Aeroelasticity Branch
AIAA Aviation 2015 ; 2015 ; Dallas, TX, United States
2015-06-22
Aufsatz (Konferenz)
Keine Angabe
Englisch
Ongoing Fixed Wing Research within the NASA Langley Aeroelasticity Branch (AIAA 2015-2719)
British Library Conference Proceedings | 2015
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