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Titel:

Shape optimization of airfoils for drag minimization over a range of operating conditions

Dokumenttyp:
Konferenzbeitrag
Art des Konferenzbeitrags:
Textbeitrag / Aufsatz
Autor(en):
Srinath, D.N.; Wall, W.A.
Abstract:
A continuous adjoint formulation is used to determine an optimal airfoil shape which has the least drag coefficient between Re = 10, 000 and 20, 000. An approach derived from concepts of robust design is employed for this purpose. A finite element method based on streamline-upwind Petrov/Galerkin (SUPG) and pressure stabilized Petrov/Galerkin (PSPG) stabilizations is used to solve both the flow and adjoint equations. The airfoil is parametrized via a Non-Uniform Rational B-Splines (NURBS)...     »
Stichworte:
Shape Optimization, Robust Design, Adjoint Methods, Airfoils
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften
Kongress- / Buchtitel:
Proceedings CFD and Optimization 2011
Kongress / Zusatzinformationen:
an ECCOMAS Thematic Conf.
Jahr:
2011
Reviewed:
ja
Sprache:
en
Erscheinungsform:
Print
Semester:
SS 11
Format:
Text
 BibTeX