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Fast Preliminary Fluid Mechanical Analysis of Fighter Aircraft Wind Tunnel Models by Application of Grid Adaptation Techniques

Zastrow, Jonas (2020) Fast Preliminary Fluid Mechanical Analysis of Fighter Aircraft Wind Tunnel Models by Application of Grid Adaptation Techniques. NATO-AVT-324 - Multi-Disciplinary Design Approaches and Performance Assessment of Future Combat Aircraft, 28.-30. Sep. 2021, online.

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Item URL in elib:https://elib.dlr.de/140250/
Document Type:Conference or Workshop Item (Speech)
Title:Fast Preliminary Fluid Mechanical Analysis of Fighter Aircraft Wind Tunnel Models by Application of Grid Adaptation Techniques
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Zastrow, Jonasjonas.zastrow (at) dlr.deUNSPECIFIED
Date:September 2020
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:combat aircraft model, grid adaptation, mesh refinement, vortex system, DLR-F23
Event Title:NATO-AVT-324 - Multi-Disciplinary Design Approaches and Performance Assessment of Future Combat Aircraft
Event Location:online
Event Type:international Conference
Event Dates:28.-30. Sep. 2021
Organizer:NATO
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: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Aeroelastic Experiments
Institute of Aeroelasticity > Aeroelastic Simulations
Deposited By: Zastrow, Jonas
Deposited On:12 Jan 2021 09:14
Last Modified:12 Jan 2021 09:14

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