Eine Auswahl der Veröffentlichungen zum Forschungsschwerpunkt "Strukturanalyse" ab 1999



2007

Rapid simulation of impacts on composite sandwich panels inducing barely visible damage
Composite Structures, Vol. 79, Issue 4, pp. 527-534
L. Kärger, J. Baaran, J. Teßmer
mehr...

Experiments on Buckling and Postbuckling of Thin-Walled CFRP Structures using Advanced Measurement Systems
International Journal of Structural Stability and Dynamics, Vol. 7, Issue 2, pp. 337-358
R. Degenhardt, A. Kling, W. Hillger, H.C.  Goetting, R. Zimmermann, K. Rohwer, A. Gleiter
mehr...

Stiffness and failure behaviour of folded sandwich cores under combined transverse shear and compression
Composites Part A, Vol. 38, Issue 5, pp.1288-1295
M. Kintscher, L. Kärger, A. Wetzel, D. Hartung
mehr...

High-performance four-node shell element with piezoelectric coupling for the analysis of smart laminated structures
International Journal for Numerical Methods in Engineering, Vol. 70 Issue 8, pp. 934-961
R. Zemcik, R. Rolfes, M. Rose, J. Teßmer
mehr... 

Development of a finite element methodology for the propagation of delaminations in composite structures
A. Orifici, R.S. Thomson, R. Degenhardt, C. Bisagni, C. J. Bayandor
Mechanics of Composite Materials, Vol. 43, Issue 1, pp. 9-28
mehr...

Probabilistic Approach for better Buckling Knock-down Factors of CFRP Cylindrical Shells - Tests and Analyses
18th Engineering Mechanics Division Conference of the American Society of Civil Engineers, Blacksburg, Virginia, USA, 3.-6.6.2007
R. Degenhardt, A. Bethge, K. Rohwer, R. Zimmermann, A. Kling

Characterisation of textile composites under combined three dimensional load conditions
3. International Conference on Computational Methods and Experiments in Material Characterisation, Bologna, Italien, 13.-15.6.2007
D. Hartung, L. Aschenbrenner, J. Teßmer

Simulating Postbuckling Behaviour and Collapse of Stiffened CFRP Panels
NAFEMS World Congress 2007, Vancouver, Kanada, 222.-25.5.2007
K. Rohwer, R. Degenhardt

Tailored Fibre Placement Technology  Optimisation and computation of CFRP structures
Advances in Design and Analysis of Composite Structures - ESAComp Users' Meeting 2007, Braunschweig, 24.-25.4.2007
L. Aschenbrenner, H. Temmen, R. Degenhardt

Structural Mechanic Aspects of CFRP Fuselage Structures
Advances in Design and Analysis of Composite Structures - ESAComp Users' Meeting 2007, Braunschweig, 24.-25.4.2007
A. Kling, J. Teßmer   

Improved Design Scenario for Composite Airframe Structures
48th AIAA Conference on Structures, Structural Dynamics and Materials, Hawaii, USA, 23-26.4.2007
R. Degenhardt, J. Teßmer

Failure and Impact Modelling of textile Composites: ITOOL Project
SAMPE Europe, 28th Intern. Conference, Paris, Frankreich, 22.-4.4.2007
B. van den Broucke, M.C. de Verdiere, D. Hartung, P. Middendorf, A. Pickett, D. Ranz Angulo, M. Schouten, J. Teßmer 

Potentials and Limitation of FE-based Simulation Methods for Fibre Composite Structures
NAFEMS Seminar Zuverlässiger Einsatz Numerischer Simulationsmethoden in der Vorausberechnung, Widerspruch  Herausforderung  Erfolgsfaktoren, Wiesbaden, Deutschland, 28.-29.3.2007 
A. Kling, L. Kärger, J. Baaran, J. Teßmer 

New Achievements in Stability of Composite Airframe Structures
12th Australian International Aerospace Congress, Melbourne, Australien, 19.-22.3.2007
R. Degenhardt, J. Teßmer

Experimental validation of efficient impact simulation methodologies of sandwich structures
12th Australian International Aerospace Congress, Melbourne, Australien, 19.-22.3.2007
L. Kärger, J. Baaran, J. Teßmer

   
Development of a Finite Element Methodology for Modelling Mixed-Mode Delamination Growth
12th Australian International Aerospace Congress, Melbourne, Australien, 19.-22.3.2007
A. Orifici, R.S. Thomson, R. Degenhardt, S. Büsing, J. Bayandor


  

2006

A three-layered sandwich element with improved transverse shear stiffness and stresses based on FSDT
Computers and Structures, Vol. 84, Issues 13-14, pp. 843-854
L. Kärger,A. Wetzel, R. Rolfes, K. Rohwer
mehr...


A semi-analytical model for local post-buckling analysis of stringer-and frame-stiffened cylindrical panels
Thin-Walled Structures, Volume 44, Issue 1, pp 102-114
P. Buermann, R. Rolfes, J. Teßmer and M. Schagerl
mehr...


POSICOSS - Improved postbuckling simulation for design of fibre composite stiffened fuselage structures
Composite Structures, Vol. 73, Issue 2, pp. 171-174
R. Zimmermann, R. Rolfes
mehr...


COCOMAT - Improved material exploitation of composite airframe structures by accurate simulation of postbuckling and collapse
Composite Structures, Volume 73, Issue 2, pp. 175-178
R. Degenhardt, R. Rolfes, R. Zimmermann, K. Rohwer
mehr...


A hybrid subspace analysis procedure for non-linear postbuckling calculation
Composite Structures, Vol 73, Issue 2, pp. 162-170
A. Kling, R. Degenhardt, R. Zimmermann
mehr...

High performance 4-node shell element for the analysis of laminated structures with piezoelectric coupling
Mechanics of Advanced Materials and Structures, Volume 13, Issue 5, pp. 393-401
R. Zemcík, R. Rolfes, M. Rose, J. Teßmer
mehr...


Thermal Analysis of Hybrid Composite Structures
ICAS 2006, 25th Congress of the International Council of the Aeronautical Sciences, Hamburg, 3.-8.9.2006
J. Teßmer, T. Spröwitz, T. Wille

Tailored Fibre Placement Optimization Tool
ICAS 2006, 25th Congress of the International Council of the Aeronautical Sciences, Hamburg, 3.-8.9.2006
H. Temmen, R. Degenhardt, T. Raible

Development and Application of a new Design Tool for aerospace Sructures
ICAS 2006, 25th Congress of the International Council of the Aeronautical Sciences, Hamburg, 3.-8.9.2006
R. Degenhardt, J. Wilhelmi, A. Grünwald

Future Design Scenario for Composite Airframe Panels
ICAS 2006, 25th Congress of the International Council of the Aeronautical Sciences, Hamburg, 3.-8.9.2006
R. Degenhardt, A. Kling, K. Rohwer

Efficient prediction of composite damage tolerance
ICAS 2006, 25th Congress of the International Council of the Aeronautical Sciences, Hamburg, 3.-8.9.2006
J. Baaran, L. Kärger, A. Wetzel

Validation procedure for Nonlinear Analysis of Stringer Stiffened CFRP Panels
ICAS 2006, 25th Congress of the International Council of the Aeronautical Sciences, Hamburg, 3.-8.9.2006
A. Kling, J. Teßmer, R. Degenhardt

Future Design for Composite Airframe Structures – The Projects POSICOSS and COCOMAT
4th International Conference on New Aerospace Trends, Bilbao, Spain, 26.-27.10.2006
R. Degenhardt

Damage Tolerance of Sandwich Structures – Modelling, Analysis and Testing
Conference on Damage in Composite Materials: Simulation and Non-Destructive Testing (CDCM 06) Stuttgart, 18.-19.9.2006
J. Teßmer

Improved Exploitation of Composite Airframe Structures by Accurate Simulation of Collapse - The COCOMAT project
Aeronautics Days, Wien, 19.-21. 6.2006
R. Degenhardt

Strength of textile Composites
3. European Conference on Computational Solid and Structural Mechanics(ECCM 2006), Lisbon, 4.-8.6.2006
Rolfes, Ernst, Hartung, Teßmer

FE-Tool CODAC for an efficient Simulation of Low-Velocity Impacts on Composite Sandwich Structures
3. European Conference on Computational Solid and Structural Mechanics(ECCM 2006), Lisbon, 4.-8.6.2006
L. Kärger, J. Baaran, J. Teßmer

Design and Analysis of Composite Panels
3. European Conference on Computational Solid and Structural Mechanics(ECCM 2006), Lisbon, 4.-8.6.2006
R. Degenhardt, A. Kling, K. Rohwer

Development of a Degradation Model for the Collapse Analysis of Composite Aerospace Structures
3. European Conference on Computational Solid and Structural Mechanics(ECCM 2006), Lisbon, 4.-8.6.2006
A. Orifici, R. Thomson, R. Degenhardt, C. Bisagni, J. Bayandor

Stiffness and Failure behaviour of folded sandwich cores under combined transverse shear and compression
CompTest 2006, 10.-12. 4.2006, Porto, Portugal
D. Hartung, M. Kintscher, L. Kärger, A. Wetzel

2005

Schnelle Rechenverfahren für Entwurf und Tragfähigkeitsnachweis

Buckling and Postbuckling Analysis of a CFRP Stiffened Panel for a Better Material Exploration
Proceedings of the SAMTECH Users Conferences, Paris, France, 2-3 February 2005
R. Degenhardt, J.-P. Delsemme

pdf pdf-file (0.3 MB)


Improved Material Exploitation of Composite Airframe Structures by Accurate Simulation of Postbuckling and Collapse – The Projects POSICOSS and COCOMAT
Proceedings of the 11th Austalian International Aerospace Congress, Melbourne, Australia, 13-17 March 2005
R. Degenhardt, R. Zimmermann, R.Rolfes, K. Rohwer

pdf pdf-file (0.1 MB)


Benchmark Finite Element Simulations of Postbuckling Composite Stiffened Panels
Proceedings of the 11th Austalian International Aerospace Congress, Melbourne, Australia, 13-17 March 2005
Orifici, A. C., Thomson, R. S., Gunnion, A. J., Degenhardt, R., Abramovich, H., Bayandor, J.

pdf pdf-file (1.0 MB)


Novel stability design scenario for aircraft structures – simulation and experimental validation
Proceedings of the 5th International Conference on Computation of Shell and Spatial Structures, Salzburg, Austria, 1-4 June, 2005
A. Kling, R. Degenhardt, H. Klein, J. Teßmer, R. Zimmermann

pdf pdf-file (0.1 MB)


3D Analysis of Couple Thin-Walled Structural Elements by Means of Standard Boundary-Element Formulations
Proceedings of the Mechanics & Materials Conference, Baton Rouge, Louisana, 1-3 June, 2005
F. C. Araújo, K. I. Silva, R. Degenhardt

pdf pdf-file (0.2 MB)


Advances in Computational Stability Analysis of Composite Aerospace Structures
Proceedings of the International Congress on FEM Technology - 23th CADFEM Users' Meeting, Bonn, Germany, 9-11 November, 2005
R. Degenhardt, J. Tessmer

pdf pdf-file (0.9 MB)


Degradation investigation in a postbuckling composite stiffened fuselage panel
Proceedings of the 13th International Conference of Composite Structures, Melbourne, Australia, 14-16 November 2005
A. C. Orifici, R. S. Thomson, R. Degenhardt, A. Kling, K. Rohwer, J. Bayandor

pdf pdf-file (0.5 MB)


2004

A Hierarchic 3D Finite Element for Laminated Composites
International Journal for Numerical Methods in Engineering, volume 6, issue 1, pp. 96-116
Kuhlmann, G., Rolfes, R.

pdf pdf-file (0.7 MB)


Analyzing Laminated Structures from Fibre-Reinforced Composite Material – An Assessment
TECHNISCHE MECHANIK, Band 25, Heft 1, (2005), 59-79
K. Rohwer, S. Friedrichs, C. Wehmeyer

pdf pdf-file (0.8 MB)


Analyzing Postbuckling Analysis of CFRP Stringer Stiffened Panels – Benchmarking and Development of Fast Tools
Proceedings of the International Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures, Eilat, Israel, March 1-2, 2004
T.Möcker, H.-G. Reimerdes, R. Degenhardt, R.Zimmermann

pdf pdf-file (0.1 MB)


Postbuckling Analysis of Fibre Composite Stringer Stiffened Panels - Development of a Fast Design Tool
Proceedings of the International Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures, Eilat, Israel, March 1-2, 2004
A. Kling, R. Degenhardt, R. Zimmermann

pdf pdf-file (2.0 MB)


COCOMAT - Improved Material Exploitation at Safe Design of Composite Airframe Structures by Accurate Simulation of Collapse
Proceedings of the International Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures, Eilat, Israel, March 1-2, 2004
R. Degenhardt, R. Rolfes, R. Zimmermann, K. Rohwer

pdf pdf-file (0.1 MB)


Postbuckling and Collapse Analysis of CFRP Stringer Stiffened Panels - a Garteur Activity
Proceedings of the 4th International Conference on Thin-Walled Structures, Loughborough, England, 22-24 June, 2004
R. Degenhardt, K. Rohwer, W. Wagner, J.-P. Delsemme

pdf pdf-file (0.5 MB)


New Design Tools for Lightweight Aerospace Structures
Proceedings of the 7th International Conference on Computational Structures Technology, Lisbon, Portugal, 7-9 September, 2004
R. Rolfes, J. Tessmer, R. Degenhardt, H. Temmen, P. Bürmann, J. Juhasz

pdf pdf-file (0.5 MB)


2003

Berechnung von Wärmeübertragungsvorgängen bei Hybridwerkstoffen - Teil II: Thermalanalyse der Rumpftonne eines Großraumflugzeuges
MSC.Virtual product Development Conference, Bad Neuenahr, 24-26.06.2003
Waitz, S., Ackva, J., Teßmer, J., Rolfes, R., de Vries, T.

pdf pdf-file (3.9 MB)

Thermal Analysis Computation and Experimental Validation of Fiber Metal Laminates
5th International Congress on Thermal Stresses and Related Topics, TS2003, Blacksburg, Virginia, USA, 8.-11.6.2003
Teßmer, J., Waitz, S., Rolfes, R., Ackva, J., de Vries, T.

pdf pdf-file (0.3 MB)

New layerwise theories and finite elements for efficient thermal analysis of hybrid structures laminates
Computers and Structures, Volume 81, Issues 26-27, pp.2525-2538
Noack, J., Rolfes, R., Teßmer, J.

pdf pdf-file (0.7 MB)

Models and Tools for Heat Transfer, Thermal Stresses and Stability of Composite Aerospace Structures
Journal of Thermal Stresses 6, p.641-670 (2003)
Rolfes, R., Rohwer, K., Teßmer, J.

pdf pdf-file (0.8 MB)


2002

High Performance Tools for Failure, Damage Tolerance and Stability Analysis of Composite Structurs
Proceedings of the Fifth World Congress on Computational Mechanics (WCCM V), Wien, 7.-12. Juli 2002
Rolfes, Baaran, Juhasz, Kling, Nolden

pdf pdf-file (1.0 MB)

Sensitivities to Geometrical and Loading Imperfections on Buckling of Composite Cylindrical Shells
Proceedings European Conference on Spacecraft Structures, Materials and Mechanical Testing, 11.-13. Dezember 2002, Toulouse
Hühne, Ch., Zimmermann, R., Rolfes, R., Geier, B.

pdf pdf-file (0.8 MB)

On the influence of laminate stacking on buckling of composite cylindrical shells subjected to axial compresssion
Composite Structures, 55/4, S. 467-474 (2002)
Geier, B., Meyer-Piening, H.-R., Zimmermann, R.

pdf pdf-file (0.8 MB)


2001

Fast Analysis Tools for Concurrent/Integrated Engineering of Composite Airframe Structures
in: Mistree, F.; Belegundu, A.D.: Optimization in Industry II, Proceedings of the International Conference on Optimization in Industry II, Banff, S. 331-338(2001)
Rolfes, R., Noack, J., Ruiz-Valdepenas, F., Taeschner, M., Zimmermann, R.

pdf pdf-file (0.3 MB)

A New Strength Model for Application of a Physically Based Failure Criterion to Orthogonal 3D Fiber Reinforced Plastics
Composites Science and Technology 61, S.1821-1832(2001)
Juhasz, J., Rolfes, R., Rohwer, K.

pdf pdf-file (0.3 MB)

Schadenstoleranz und Schwingfestigkeit neuer textiler Faserverbunde für Hochleistungsstrukturen: Experiment und Simulation
in: Fertigungsverfahren und Betriebsfestigkeit, 28. Tagung des DVM-Arbeitskreises Betriebsfestigkeit, Deutscher Verband für Materialforschung und -prüfung e.V., S.339-348(2001)
Baaran, J., Gädke, M., Goetting, H.-C., Rolfes, R.

CFRP Fuselage Structures - Postbuckling Permitted
Air & Space Europe, Vol. 3, Nr. 3/4, 2001, pp. 129-131.
Zimmermann, R., Rolfes, R.

pdf pdf-file (0.2 MB)

Buckling Loads of CFRP Composite Cylinders under Combined Axial and Torsion Loading - Experiments and Computations
Composite Structures, Vol. 53, 2001, pp. 420-435.
Meyer-Piening, H.-R.a , Farshad, M.b , Geier, B., Zimmermann, R.
a ETH Zürich, b EMPA Dübendorf

pdf pdf-file (0.9MB)

Impact Behavior and Residual Strength of Sandwich Structural Elements Under Static and Fatigue Loading
42nd AIAA/ASME/ASCE/AHS/ASC,Structures, Structural Dynamics, and Materials Conference and Exhibit, Seattle, Washington, 16.-19. April 2001
Gädke, M., Baaran, J., Goetting, H.-C., Rolfes, R.

pdf pdf-file (0.8MB)

Thermo-mechanical design aspects for primary composite structures of large transport aircraft
Aerosp. Sci. Technol. (AST), 5, (2001), S. 135-146
Petersen, D., Rolfes, R., Zimmermann, R.

pdf pdf-file (0.5 MB)

Higher-order theories for thermal stresses in layered plates
Solids and Structures 38,(2001), S. 3673-3687
Rohwer, K., Rolfes, R., Sparr, H.

pdf pdf-file (0.6 MB)

Fast and Reliable Development of Composite Structures Using Concurrent/Integrated Engineering
Aeronautics Days 2001, Hamburg, 29.-31.Januar 2001, European Commission, Community research, Book of Abstracts, Aeronautics Days 2001 "Preparing for the Global Challenges", S. 169-169, (2001)
Rolfes, R., Baaran, J., Juhasz, J., Nolden, P., Teßmer, J., et al.

2D Finite Element Formulation for 3D Temperature Analysis of Layered Hybrid Structures
NAFEMS-Seminar: "Numerical Simulation of Heat Transfer", Wiesbaden, 9./10.5.2001, NAFEMS, Seminar: Numerical Simulation of Heat Transfer, S. 1-5, (2001)
Rolfes, R., Tessmer, J.

pdf pdf-file (0.8 MB)

Nachbeulverhalten von Flugzeugrumpfschalen
Proceedings of the 13th German ABAQUS User Conference, Freiburg, Germany, 24-25 September, 2001
Kling, A., Degenhardt, R.

pdf pdf-file (0.3 MB)


2000

Advanced Analysis Tools for Concurrent/Integrated Engineering of Composite Airframe Structures
Proceedings of the 1st Stade Composite Colloquium, 7.-8. Sept. 2000, S.225-243
Rolfes, Baaran, Juhasz, Nolden, Teßmer, Töpfer, Zimmermann

pdf pdf-file (0.3 MB)

Damage tolerance of composite structures for large transport aircraft
Aerospace Science and Technology, 4, 1, (2000), S. 23-32
Gädke, M., Roudolff, F.

Integrated Thermal and Mechanical Analysis of Composite Plates and Shells
Composites Science and Technology 60, 11, (2000), S. 2097-2106
Rolfes, R., Rohwer, K.

pdf pdf-file (0.8 MB)

1999

High Performance 3D-Analysis of Thermo-Mechanically Loaded Composite Structures
Composite Structures 46, S. 367-379 (1999)
Rolfes, R., Noack, J., Taeschner, M.

pdf pdf-file (1.1 MB)

Buckling of Axially Compressed Fiber Composite Cylindrical Shells due to Impulsive Loading
Conference on Spacecraft Structures, Materials & Mechanical Testing, Braunschweig, Germany, 04-06 November 1998, Proceedings (ESA SP-428, February 1999), p.557-562
Bisagni, C., Zimmermann, R.

Development and Experimental Verification of FE-Model for Stringer-Stiffened Fibre Composite Panels under Combined Thermal and Mechanical Loading Conditions
European Conference on Spacecraft Structures, Materials, and Mechanical Testing, 4.-6. November 1998, Braunschweig, ESA SP-428, pp.117-122(1999)
Rolfes, R., Tacke, S., Zimmermann, R.

pdf pdf-file (0.4 MB)

Efficient Thermal Analysis of Hot Structures Using New Finite Elements
European Conference on Spacecraft Structures, Materials, and Mechanical Testing, 4.-6. November 1998, Braunschweig, ESA SP-428, pp.117-122(1999)
Noack, J.; Rolfes, R.

The Imperfection Sensitivity of Axially Compressed Thin-Walled Circular Cylinders - Attempts to Define a Measure
39th AIAA/ASME/ASCE/AHS/ASC Structural Dynamics and Materials Conference, Long Beach, CA, April 1998, Paper AIAA 98-1771
Geier, B.

Integration und Qualifikation

2003

Virtual Testing of Aircraft Structures, considering Postcritical and Thermal Behavior
Composit Thematic Network Workshop on Modeling and Prediction of Composite Transport Structures, Zaragoza, Spain, 30.06.2003
Teßmer, J., Degenhardt, R., Kling, A., Rolfes, R., Spröwitz, T., Waitz, S.

pdf pdf-file (2.6 MB)

Composite Stiffened Panel Impact Damage Simulations And Parametric Studies
Mee, David J. (Hrsg.): Proceedings of the 10th Australian International Aerospace Congress, 29.-31 Juli 2003, Brisbane, ISBN 085-825-733-5 (2003)
Rolfes, Yap, Scott, Hachenberg, Baaran.

pdf pdf-file (0.4 MB)

Umsetzung eines BOOSTER DAAR-Ringes in Faserverbundweise für die ARIANE 5 Trägerrakete
Deutscher Luft- und Raumfahrtkongress 2003, Deutsche Gesellschaft für Luft- und Raumfahrt, München, Deutschland, 17. 11. 2003
Niederstadt, Hühne, Kolesnikov, Reinhold, Kleineberg
pdf pdf-file (0.4 MB)



2001

Thermo-mechanical design aspects for primary composite structures of large transport aircraft
Aerospace Science Technologies 5, p.135-146 (2001)
Petersen, D., Rolfes, R., Zimmermann, R.

pdf pdf-file (0.5 MB)

Recent Thermo-mechanical Test Series and Innovative Test Procedures
European Conference on Spacecraft Structures, Materials and Mechanical Testing, Noordwijk, Netherlands, 29.11.-1-12.2000, ESA, Proceedings of the European Conference on Spacecraft Structures, Materials and Mechanical Testing,, S. 409-414, ESA, (2001)
Petersen, D., Klein, H., Hildebrand, B.

2000

Festigkeit von Faserverbunden unter zügiger und schwingender Belastung
Seminar TV 2.02 Entwurf, Berechnung und Fertigung von Leichtbaustrukturen aus Faserverbundwerkstoff, Braunschweig, 28.-30.11.2000, Carl Cranz Gesellschaft, Entwurf, Berechnung und Fertigung von Leichtbaustrukturen aus Faserverbundwerkstoffen, S. 1-136, (2000)
Goetting, H.-C., Gädke, M.

Festigkeit von Faserverbunden unter zügiger und schwingender Belastung: Teil 1
Seminar TV 2.02 Entwurf, Berechnung und Fertigung von Leichtbaustrukturen aus Faserverbundwerkstoff, Braunschweig, 28.-30.11.2000, Carl Cranz Gesellschaft, Entwurf, Berechnung und Fertigung von Leichtbaustrukturen aus Faserverbundwerkstoffen, S. 1-147, (2000)
Goetting, H.-C., Gädke, M.

Development of Encapsulated PZT-Patches for Adaptive Structures
Adaptronic Congress, Potsdam, 4.4.-5.4.2000, Adaptronic Congress Veranstaltungs GbR, Adaptronic Congress Conference Proceedings, S. 91-95, (2000)
Wierach, P., Goetting, H. C., Schönecker, A.

1999

Thermo-Mechanical Behaviour of Large Transport Aircraft Structures
ONERA-DLR Symposium, Paris, 21-27 June 1999
Petersen, D., Rolfes, R., Noack, J., Hildebrandt, B.

Thermo-Mechanical Test Procedures for X-38 Rudder
International Symposium Atmospheric Reentry Vehicles and Systems, Arcachon, France, 16-18 March 1999
Petersen, D., Klein, H., Schmidt, K., Kepke, M., Hildebrandt, B.

Lightweight Composite Feedlines for Future Launchers
European Conference on Spacecraft Structures, Materials, and Mechanical Testing, 4.-6. November 1998, Braunschweig, Tagungsband erscheint in 1999
Netz, P., Rolfes, R.

Schadensdetektion und Ultraschall

2002

Inspection of CFRP Components by Ultrasonic Imaging with Air Coupling
8th ECNDT Barcelona 2002, Technical Papers
Hillger, W., Meier, R., Henrich, R.

pdf pdf-file (0.6 MB)

Determination of Porosity in Aerospace Structures by Ultrasonic Pulse Echo Technique
8th ECNDT Barcelona 2002, Technical Papers
Hillger, W., Elze, S.

pdf pdf-file (0.3 MB)

Ultraschallprüftechnik zur Porositätsbestimmung in CFK-Bauteilen
DGzfP-Jahrestagung 2002, Weimar, 6.-8. Mai 2002, Berichtsband
Hillger, W., Elze, S., Henrich, R.

pdf pdf-file (0.4 MB)

2000

Ultrasonic Testing of Composites - from Laboratory Research to Field Inspections
15th World Conference on Nondestructive Testing, Rom, 15.-21. October 2000
Hillger, W.

pdf pdf-file (0.3 MB)

Erfahrungen mit luftgekoppelter Ultraschallprüftechnik
DGzfP-Jahrestagung 2000, Innsbruck, 29.-31. 05. 2000, DGzfP, Jahrestagung 2000 - Zerstörungsfreie Materialprüfung, S. 781-786, DGzfP, (2000)
Hillger, W.

pdf pdf-file (0.3 MB)

1999

AirTech - ein neues Ultraschallprüfsystem mit Ankopplung über Luft
Vortrag P11, DGZfP- Jahrestagung 1999, Celle, Berichtsband 68, Band 2, S. 641-648
Hillger, W.

pdf pdf-file (0.4 MB)

Bildgebende Ultraschallprüfung an CFK-Probekörpern mit Ankopplung über Luft
Vortrag 26, DGZfP-Jahrestagung 1999, Berichtsband 68, Band 1, S. 243-250
Hillger, W., Gebhardt, W.

pdf pdf-file (0.3 MB)


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