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Comparison between VLM and CFD maneuver loads calculation at the example of a flying wing configuration

Voß, Arne (2019) Comparison between VLM and CFD maneuver loads calculation at the example of a flying wing configuration. Journal of Aeroelasticity and Structural Dynamics, pp. 19-37. Department of Aerospace Engineering of Politecnico di Milano. DOI: 10.3293/asdj.2019.52 ISSN 1974-5117

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Official URL: https://www.asdjournal.org/index.php/ASD/article/view/52

Abstract

This work presents the results of computational fluid dynamics (CFD) based maneuver loads calculations for a flying wing configuration. Euler solutions of the DLR Tau code are compared to vortex lattice method (VLM) results for maneuver loads in the preliminary design stage. The trim parameters of the quasi-steady maneuver load case, the structural deformation and the flow solution are determined in an iterative process. The focus is on a comprehensive loads analysis including a broad selection of load cases to cover the whole flight envelope. This is necessary to ensure a thorough preliminary design. Integration of this approach in an automated, preliminary design process and application of parametric, aeroelastic modeling allows to perform structural optimization loops to evaluate the difference between VLM and CFD on the structural design in terms of structural net mass.

Item URL in elib:https://elib.dlr.de/133173/
Document Type:Article
Title:Comparison between VLM and CFD maneuver loads calculation at the example of a flying wing configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Voß, ArneArne.Voss (at) dlr.dehttps://orcid.org/0000-0003-2266-7853
Date:30 December 2019
Journal or Publication Title:Journal of Aeroelasticity and Structural Dynamics
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.3293/asdj.2019.52
Page Range:pp. 19-37
Publisher:Department of Aerospace Engineering of Politecnico di Milano
ISSN:1974-5117
Status:Published
Keywords:Flying wing, maneuver loads, aeroelasticity, VLM, CFD
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 - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Voß, Arne
Deposited On:06 Jan 2020 16:31
Last Modified:06 Jan 2020 16:31

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