Change search
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf
Aircraft composites and aeroelastic tailoring
KTH, Superseded Departments, Aeronautical Engineering.ORCID iD: 0000-0003-3337-1900
1998 (English)Doctoral thesis, comprehensive summary (Other scientific)
Abstract [en]

This thesis treats various aspects of structural polymercomposites in aircraft applications. The mechanical performanceand quality of resin transfer molded (RTM) carbon fiberreinforced epoxy composites is studied. In a first part, the influence of manufacturing process parameters on the mechanicalbehavior of laminates is experimentally investigated. A number of process parameters are used as variables and performance ismeasured in terms of tensile and compressive strength as wellas interlaminar fracture toughness. The process parameters are concluded to have little affect on the measured properties. In a second part, the quality and structural performance of an entirely co-cured RTM manufactured aircraft control surfacedemonstrator is investigated. A series of quasi staticstructural tests using distributed loading is performed. Experimental results are compared with finite element analysis. Effects of impact damage on the performance are also studied.Good agreement is obtained between the predictions and the experiments.

A nondestructive method for determination of elasticmaterial properties of orthotropic plates using naturalfrequencies is developed and verified. Finite elementcalculations of the natural frequencies of the plate are matched to experimentally determined frequencies using theelastic constants as variables. The method is successfully verified even for nontrivial specimen geometries with cornersingularities. Emphasis is on practical utilization ofknowledge about numerical and modeling errors as well asexperimental uncertainties.

The optimal design of a thin orthotropic wing subject toaeroelastic constraints is studied using numerical methods andverified in low speed wind tunnel testing. The flutter speed ofthe wing is maximized using the laminate orientation asvariable. Further, the problem of increasing the flutter speed to a prescribed value using minimal amount of additional concentrated masses on a  fixed wing design is investigated. The main objective of the study is to verify that the performance of the optimized design can be achieved also in experiments. It is found that the optimal design is very sensitive to uncertainties in material and structural properties.Consequently, this has to be accounted for in the problemformulation. It is shown, and experimentally verified, that the robustness requirements on the optimal design can be met byreformulating the optimization problem.

Place, publisher, year, edition, pages
Stockholm: KTH , 1998. , vii, 23 p.
Series
Report. Department of Aeronautics, 98:13
Keyword [en]
polymer composites, testing, resin, transfer molding, RTM, process parameters, mechanical properties, aircraft, impact damage, BVID, modal, inverse method, uncertainties, aeroelasticity, optimization, wind tunnel
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:kth:diva-2641ISBN: 99-2600481-4 OAI: oai:DiVA.org:kth-2641DiVA: diva2:8308
Public defence
1998-05-20, 00:00 (English)
Note
QC 20100511Available from: 2000-01-01 Created: 2000-01-01 Last updated: 2010-05-11Bibliographically approved
List of papers
1. Influence of process parameters on mechanical behavior of RTM moldings
Open this publication in new window or tab >>Influence of process parameters on mechanical behavior of RTM moldings
1995 (English)In: Tenth International Conference on Composite Materials: III. Processing and Manufacturing; Whistler, British Columbia; Canada; 14-18 Aug. 1995., 1995, 261-268 p.Conference paper, Published paper (Other academic)
Keyword
Aircraft components, Molding (process), Resin transfer molding, Epoxy resins, Composite materials, Carbon fiber reinforced plastics, Mechanical properties, Fracture toughness, Processing effects, Moldings, Interfacial shear strength, Tensile strength, Notch strength, Compressive strength, Delaminating
National Category
Engineering and Technology
Identifiers
urn:nbn:se:kth:diva-12797 (URN)
Note
QC 20100511Available from: 2010-05-11 Created: 2010-05-11 Last updated: 2010-05-11Bibliographically approved
2. Performance and quality of a resin transfer molded aircraft control surface
Open this publication in new window or tab >>Performance and quality of a resin transfer molded aircraft control surface
1995 (English)Report (Other academic)
National Category
Engineering and Technology
Identifiers
urn:nbn:se:kth:diva-12807 (URN)
Note
QC 20100511Available from: 2010-05-11 Created: 2010-05-11 Last updated: 2010-05-11Bibliographically approved
3. A finite element based modal method for determination of plate stiffnesses considering uncertainties
Open this publication in new window or tab >>A finite element based modal method for determination of plate stiffnesses considering uncertainties
1999 (English)In: Journal of composite materials, ISSN 0021-9983, E-ISSN 1530-793X, Vol. 33, no 8, 695-711 p.Article in journal (Refereed) Published
Keyword
composite, testing, orthotropic, stiffness, experimental, modal, finite element, uncertainties, corner singularity, CONSTANTS
Identifiers
urn:nbn:se:kth:diva-12799 (URN)000080242400003 ()
Note
QC 20100511Available from: 2010-05-11 Created: 2010-05-11 Last updated: 2017-12-12Bibliographically approved
4. Aeroelastic design optimization with experimental verification
Open this publication in new window or tab >>Aeroelastic design optimization with experimental verification
1998 (English)In: Journal of Aircraft, ISSN 0021-8669, E-ISSN 1533-3868, Vol. 35, no 3, 505-507 p.Article in journal (Refereed) Published
Identifiers
urn:nbn:se:kth:diva-12801 (URN)000073896600025 ()
Note
QC 20100511Available from: 2010-05-11 Created: 2010-05-11 Last updated: 2017-12-12Bibliographically approved
5. Aeroelastic tailoring considering uncertainties in material properties
Open this publication in new window or tab >>Aeroelastic tailoring considering uncertainties in material properties
1998 (English)In: Structural optimization (Print), ISSN 0934-4373, E-ISSN 1436-2503, Vol. 15, no 3-4, 157-162 p.Article in journal (Refereed) Published
National Category
Engineering and Technology
Identifiers
urn:nbn:se:kth:diva-12800 (URN)000075687400002 ()
Note
QC 20100511Available from: 2010-05-11 Created: 2010-05-11 Last updated: 2017-12-12Bibliographically approved

Open Access in DiVA

No full text

Authority records BETA

Kuttenkeuler, Jakob

Search in DiVA

By author/editor
Kuttenkeuler, Jakob
By organisation
Aeronautical Engineering
Engineering and Technology

Search outside of DiVA

GoogleGoogle Scholar

isbn
urn-nbn

Altmetric score

isbn
urn-nbn
Total: 673 hits
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf