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Dokumenttyp:
Konferenzbeitrag
Art des Konferenzbeitrags:
Textbeitrag / Aufsatz
Autor(en):
Srinath, D.N.; Wall, W.A.
Titel:
Airfoil shape optimization under a range of operating conditions
Seitenangaben Beitrag:
CD-ROM 408
Abstract:
A continuous adjoint formulation is used to determine optimal airfoil configurations 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) curve. L-BFGS algorithm is used...     »
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften
Kongress- / Buchtitel:
Proceedings 4th European Conference for Aerospace Sciences
Kongress / Zusatzinformationen:
EUCASS 2011
Jahr:
2011
Reviewed:
ja
Sprache:
en
Erscheinungsform:
CD-ROM / DVD
Semester:
SS 11
Format:
Text
 BibTeX