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Effect of Shape Parameterization and Optimization Algorithms on Adjoint Based Aerodynamic Shape Optimization
A very important phase in aircraft design is the aerodynamic design of the wing and
various other components: wing-body fairing, tailplane, etc. With today’s computer
power and progress in algorithm development, the design is made through complex
mathematical models which are amenable to automatic optimization. An industrial
adjoint-based three-dimensional viscous optimization framework, developed at
Bombardier Aerospace, will be made more efficient by performing code-to-code
validation with research codes at UTIAS. Improvements in all area of the framework
will be examined, ie. aerodynamic parameterization, mesh movement and optimization
algorithms. The importance of overall robustness of the framework will be
demonstrated on test cases. The benefits will be to increase the t
Faculty Supervisor:
David Zingg
Student:
Partner:
Bombardier Aerospace Inc (Dorval, QC)
Discipline:
Engineering
Sector:
Manufacturing; Transportation and warehousing
University:
University of Toronto
Program:
Accelerate
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