Aerodynamic optimization of turboprop turbine blades using a response surface methodology based algorithm

Tosin, Stefano; Friedrichs, Jens; Sperling, Johann; Kožulović, Dragan

doi:10.1115/FEDSM2014-21752

Verlagslink DOI:	10.1115/FEDSM2014-21752
Titel:	Aerodynamic optimization of turboprop turbine blades using a response surface methodology based algorithm
Sprache:	Englisch
Autorenschaft:	Tosin, Stefano Friedrichs, Jens Sperling, Johann Kožulović, Dragan
Herausgeber:	American Society of Mechanical Engineers. Fluids Engineering Division
Erscheinungsdatum:	2014
Verlag:	ASME
Quellenangabe:	Teil: Advances in fluids engineering education, turbomachinery flow prediction and optimization, applications in CFD, bio-inspired fluid mechanics, droplet-surface interactions, CFD verification and validation, development and applications of immersed boundary methods, DNS, LES, and hybrid RANS/LES methods
Teil der Schriftenreihe:	Proceedings of the ASME Fluids Engineering Division summer meeting - 2014 : presented at the ASME 2014 4th Joint US-European Fluids Engineering Division Summer Meeting; August 3 - 7, 2014, Chicago, Illinois, USA
Bandangabe:	Vol. 1A : Symposia
Zeitschrift oder Schriftenreihe:	FED
Konferenz:	ASME Joint US-European Fluids Engineering Division Summer Meeting 2014
URI:	http://hdl.handle.net/20.500.12738/12708
ISBN:	9780791846216
ISSN:	0888-8116
Einrichtung:	Department Fahrzeugtechnik und Flugzeugbau Forschungs- und Transferzentrum Future Air Mobility Fakultät Technik und Informatik
Dokumenttyp:	Chapter/Article (Proceedings)
Appears in Collections:	Publications without full text