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Three-parameter uncertainty quantification for generic missile FG5

Peter, Jacques and Görtz, Stefan and Graves, Rick (2017) Three-parameter uncertainty quantification for generic missile FG5. In: 55th AIAA Aerospace Sciences Meeting. AIAA Science and Technology Forum and Exposition, 09.-13. Jan. 2017, Grapevine, USA. DOI: 10.2514/6.2017-1197

Full text not available from this repository.

Official URL: http://dx.doi.org/10.2514/6.2017-1197

Abstract

This paper summarizes the results of international collaborative work on applying numerical methods for uncertainty quantification to a generic missile configuration. This work was conducted as part of the NATO STO Task Group AVT-191 on Application of Sensitivity Analysis and Uncertainty Quantification to Military Vehicle Design. Three different CFD codes are used by the three partners to compute and compare the nominal flow around the FG5 missile for which experimental data is available before moving on to estimate the statistics in output quantities of interest due prescribed uncertainty in three input parameters using different non-intrusive approaches.

Item URL in elib:https://elib.dlr.de/110345/
Document Type:Conference or Workshop Item (Speech)
Title:Three-parameter uncertainty quantification for generic missile FG5
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Peter, JacquesONERAUNSPECIFIED
Görtz, Stefanstefan.goertz (at) dlr.deUNSPECIFIED
Graves, RickUSAFRLUNSPECIFIED
Date:11 January 2017
Journal or Publication Title:55th AIAA Aerospace Sciences Meeting
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2017-1197
Status:Published
Keywords:uncertainty quantification, generic missile, CFD, aerodynamics, statistics
Event Title:AIAA Science and Technology Forum and Exposition
Event Location:Grapevine, USA
Event Type:international Conference
Event Dates:09.-13. Jan. 2017
Organizer:AIAA
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
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Deposited By: Görtz, Stefan
Deposited On:17 Jan 2017 13:55
Last Modified:17 Jan 2017 13:55

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