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UID:0-359@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20181105T163000

DTEND;TZID=Asia/Jerusalem:20181105T173000

DTSTAMP:20230527T135559Z

URL:https://aerospace.technion.ac.il/events/green-aircraft-technologies-me
 thodologies-and-results/

SUMMARY:Green Aircraft Technologies Methodologies and Results
DESCRIPTION:Lecturer:Prof. Ruxandra Mihaela Botez\n Faculty:École de Techn
 ologie Supérieure\n Institute:University of Quebec\, Montréal\, Canada\n
  Location:Classroom 165\, ground floor\, Library\, Aerospace Eng.\n Zoom: 
 \n Abstract: \n Details: \n Two main research projects that are developed 
 at the Applied Research Laboratory in Active Controls\, Avionics and AeroS
 ervoElasticity LARCASE are presented in the area of green aircraft technol
 ogies. In the first research project\, three sub-projects will be presente
 d in the area of green aircraft modeling and simulation based on flight te
 sts: 1) the development of a high-fidelity simulation model of the Cessna 
 Citation X that is efficient\, flexible and responsive for the needs of th
 e research in aerospace\, 2) aircraft parameter estimation from flight tes
 ts\, and 3) the aircraft trajectory prediction using the aero-propulsive m
 odel derived from flight tests. This research was realized thanks to the R
 esearch Aircraft Flight Simulator (RAFS) that is equipped with the flight 
 dynamics certified at the highest Level D for one of the fastest business 
 jet aircraft Cessna Citation X. The aim of this first research project is 
 to demonstrate a valid methodology that could be used in the Aerospace Ind
 ustry with the aim to reduce the number of flight tests (thus\, their cost
 s) needed to validate the aircraft models.\nIn the second multidisciplinar
 y project\, two sub-projects will be presented in the area of morphing win
 g for green aircraft technologies development. In both projects\, a differ
 ent morphing wing was designed and manufactured with the aim to reduce dra
 g and to delay the flow transition\, therefore the fuel consumption\; the 
 morphing wing was equipped in both sub-projects with piezoelectric pressur
 e sensors. The morphing wing shapes were changed using different types of 
 actuation systems\, as detailed for each sub-project: 1) classical wing-bo
 x equipped with smart material actuators\, and 2) regional jet wing equipp
 ed with in-house electrical actuators. The multidisciplinary (aerodynamics
 \, structural and controls) research methodologies and results will be pre
 sented. All these projects are realized in collaboration with Canadian aer
 ospace companies.
CATEGORIES:Seminars
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng.

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