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UID:0-218@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20211020T133000

DTEND;TZID=Asia/Jerusalem:20211020T143000

DTSTAMP:20230403T143501Z

URL:https://aerospace.technion.ac.il/events/an-experimental-aeroelastic-be
 nchmark-of-a-very-flexible-wing/

SUMMARY:An Experimental Aeroelastic Benchmark of a Very Flexible Wing
DESCRIPTION:Lecturer:Or Avin\n Faculty:Design and Manufacturing Management\
 n Institute:Technion – Israel Institute of Technology\n Location:Classro
 om 165\, ground floor\, Library\, Aerospace Eng. & https://technion.zoom.u
 s/j/95043873801\n Zoom: \n Abstract: \n Details: \n The progress towards l
 ighter and more efficient aircraft structures has led to some very flexibl
 e wing configurations that deform to a great extent under flight loads. Su
 ch designs experience unique aeroelastic phenomena that the industry-stand
 ard linear structural and aeroelastic models might not accurately predict.
  In recent years\, there has been an ongoing effort in the aeroelasticity 
 community to develop novel nonlinear models in both the structure and aero
 dynamic disciplines to analyze very flexible configurations. These models 
 require validation\, which calls for aeroelastic wind tunnel or flight tes
 ts. Aeroelastic wind tunnel tests can be used to assess the accuracy and v
 alidity of computational models and point to new physics.\nThe seminar wil
 l present the design\, analyses\, and wind-tunnel testing of the Pazy wing
  -  a very flexible wing model designed to study nonlinear aeroelastic ph
 enomena due to geometrically large deflections. Wind tunnel tests were con
 ducted at the Faculty of Aerospace Engineering subsonic wind tunnel in con
 ditions that lead to static and dynamic\, stable and unstable\, responses.
  At extreme conditions\, static deformations of 50% span were recorded\, a
 s well as instances of limit-cycle oscillations.
CATEGORIES:Seminars
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng. & https://
 technion.zoom.us/j/95043873801

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