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Validation of FEA results by results of aero-thermal testing. Aero-Thermodynamic Loads on Lightweight Advanced Structures - ATLLAS II. D3.1.9. Final Report.

Kasperovich, Galina (2016) Validation of FEA results by results of aero-thermal testing. Aero-Thermodynamic Loads on Lightweight Advanced Structures - ATLLAS II. D3.1.9. Final Report. Project Report. ACP0-GA-2010-263913, D3.1.9, 23 S. European Commission within the Seventh Framework Programme.

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Abstract

The numerical FEA model of the “CANARD” designed from TMC material by TISICS for the aero-thermal tests using the L3K facility was considered within the frame of the ATLLAS II project. As a final specification for the CANARD model, the cooling cores with exit slit geometries providing the most efficient impingement cooling effect inside of the TMC CANARD were considered for manufacture and testing. The calculations of the temperature fields, strains and stresses in the TMC part were conducted for a 0.8 mm CANARD leading edge radius according to the heat flux density provided by DLR AS-HYP. EN3B steel was examined as a cooling core material. The results are presented, discussed and compared with the experimental data received by thermal tests using the L3K facility.

Item URL in elib:https://elib.dlr.de/107507/
Document Type:Monograph (Project Report)
Title:Validation of FEA results by results of aero-thermal testing. Aero-Thermodynamic Loads on Lightweight Advanced Structures - ATLLAS II. D3.1.9. Final Report.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kasperovich, GalinaGalina.Kasperovich (at) dlr.deUNSPECIFIED
Date:2016
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:23
Publisher:European Commission within the Seventh Framework Programme
Status:Published
Keywords:FEA model, TMC material, aero-thermal tests
Institution:Institute of Materials Research
Department:Hybrid Materials Systems and Intermetallics
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 - Structures and Materials, L - Simulation and Validation
Location: Köln-Porz
Institutes and Institutions:Institute of Materials Research > Metallic Structures and Hybrid Material Systems
Deposited By: Kasperovich, Dr.-Ing. Galina
Deposited On:24 Nov 2016 11:35
Last Modified:31 Jul 2019 20:04

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