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Memorias de investigación
Communications at congresses:
Automated 3D Design of Low Pressure Turbine Airfoils Using a GPU Accelerated Adjoint Method
Year:2017
Research Areas
  • Engineering
Information
Abstract
A methodology for the full three dimensional automatic design of turbomachinery airfoils is presented, developed with the requirement of minimal output time. This requirement leads to the use of a gradient based algorithm, where derivatives are computed using the adjoint method. Where possible, the computational advantages of Graphics Processing Units have been used, qualitatively and quantitatively assessing the benefits of this approach. In order to illustrate the capabilities of the system, a Low Pressure Turbine vane has been redesigned, taking into consideration a set of rigorous design criteria.
International
Si
Congress
12th European Turbomachinery Conference
960
Place
Estocolmo
Reviewers
Si
ISBN/ISSN
CDP08UPM
Start Date
03/04/2017
End Date
07/04/2017
From page
1
To page
12
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Participants
  • Autor: Ricardo Puente Rico (UPM)
  • Autor: Roque Corral Garcia (UPM)
Research Group, Departaments and Institutes related
  • Creador: Departamento: Mecánica de Fluidos y Propulsión Aeroespacial
S2i 2020 Observatorio de investigación @ UPM con la colaboración del Consejo Social UPM
Cofinanciación del MINECO en el marco del Programa INNCIDE 2011 (OTR-2011-0236)
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