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Aerodynamic Inverse Design Framework using Discrete Adjoint Method

Brezillon, Joel and Abu-Zurayk, Mohammad (2010) Aerodynamic Inverse Design Framework using Discrete Adjoint Method. 17. DGLR / STAB Fachsymposium, 2010-11-09 - 2010-11-10, Berlin, Deutschland.

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Item URL in elib:https://elib.dlr.de/95737/
Document Type:Conference or Workshop Item (Speech)
Title:Aerodynamic Inverse Design Framework using Discrete Adjoint Method
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Brezillon, JoelUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Abu-Zurayk, Mohammadmohammed.abu-zurayk (at) dlr.deUNSPECIFIEDUNSPECIFIED
Date:2010
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:2010
Page Range:pp. 184-185
Series Name:STAB-Mitteilung
Status:Published
Keywords:Inverse design, Adjoint, CFD, Parametrisation, Optimisation
Event Title:17. DGLR / STAB Fachsymposium
Event Location:Berlin, Deutschland
Event Type:national Conference
Event Start Date:9 November 2010
Event End Date:10 November 2010
Organizer:STAB
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Seyfried, Beate
Deposited On:24 Mar 2015 16:04
Last Modified:24 Apr 2024 20:01

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