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Weight estimation report

Toso, Yves and Toso, Nathalie and Haase, Thomas (2021) Weight estimation report. Project Report. 27 S.

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Abstract

This deliverable contains the main material card data for the investigated materials Al2024T3, UD T700/M21, tri-axially braided AS4c carbon fibre reinforced M36 epoxy and tri-axially braided Zylon AS fibre reinforced Cycom 890 used for the high velocity impact simulations, the description of the chosen high velocity impact simulation approaches for the different materials, the validation of these simulations against selected high velocity impact test results and a very preliminary sizing of a fuselage skin for the load case "high velocity impact of a generic blade on a fuselage skin".

Item URL in elib:https://elib.dlr.de/147892/
Document Type:Monograph (Project Report)
Title:Weight estimation report
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Toso, YvesUNSPECIFIEDUNSPECIFIED
Toso, NathalieUNSPECIFIEDhttps://orcid.org/0000-0003-2803-1450
Haase, ThomasUNSPECIFIEDhttps://orcid.org/0000-0002-9553-9628
Date:16 December 2021
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:27
Status:Published
Keywords:high velocity impact, Al2024T3, UD T700/M21, AS4c/M36, Zylon/Cycom890, blade impact
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Components and Systems
DLR - Research area:Aeronautics
DLR - Program:L CS - Components and Systems
DLR - Research theme (Project):L - Structural Materials and Design
Location: Braunschweig , Stuttgart
Institutes and Institutions:Institute of Structures and Design > Structural Integrity
Executive Board Aeronautics and Energy Research and Technology > Program Directorate Aeronautics
Deposited By: Toso, Dr. Yves
Deposited On:11 Jan 2022 14:41
Last Modified:11 Jan 2022 14:41

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