A CONTINUOUS ADJOINT FORMULATION WITH EMPHASIS TO AERODYNAMIC-TURBOMACHINERY OPTIMIZATION

Papadimitriou, D; Giannakoglou, K

dc.contributor.author	Papadimitriou, D	en
dc.contributor.author	Giannakoglou, K	en
dc.date.accessioned	2014-03-01T01:54:48Z
dc.date.available	2014-03-01T01:54:48Z
dc.date.issued	2006	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/27471
dc.relation.uri	http://147.102.55.162/research/pdfs/3_082.pdf	en
dc.relation.uri	http://velos0.ltt.mech.ntua.gr/research/pdfs/3_082.pdf	en
dc.relation.uri	http://proceedings.fyper.com/eccomascfd2006/documents/499.pdf	en
dc.subject	Adjoint Method	en
dc.subject	Compressible Fluid Flow	en
dc.subject	Design Optimization	en
dc.subject	Entropy Generation	en
dc.subject	Function Fields	en
dc.subject	Objective Function	en
dc.subject	Shape Optimization	en
dc.subject	Test Bed	en
dc.subject	Unstructured Grid	en
dc.subject	Second Order	en
dc.title	A CONTINUOUS ADJOINT FORMULATION WITH EMPHASIS TO AERODYNAMIC-TURBOMACHINERY OPTIMIZATION	en
heal.type	journalArticle	en
heal.publicationDate	2006	en
heal.abstract	This paper summarizes progress, recently made in the Lab. of Thermal Tur- bomachines of NTUA, on the formulation and use of the continuous adjoint methods in aerodynamic shape optimization problems. The basic features of state of the art adjoint methods and tools which are capable of handling arbitrary objective functions, cast in the form of either boundary or field integrals,	en