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Scopus Author ID: 12144431600

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Employment (2)

University of Bremen: Bremen, DE

2019-02-01 to present | Professor (Faserinstitut Bremen e.V.)
Employment
Source: Self-asserted source
Richard Degenhardt

Deutsches Zentrum für Luft- und Raumfahrt Standort Braunschweig: Braunschweig, Niedersachsen, DE

2000-09-01 to present | Senior scientist (Institute of Composite Structures and Addaptive Systems)
Employment
Source: Self-asserted source
Richard Degenhardt

Education and qualifications (2)

Braunschweig University of Technology: Braunschweig, DE

1990-12-01 to 1996-03-31 | PhD student (Institute of Applied Mechanics)
Qualification
Source: Self-asserted source
Richard Degenhardt

Braunschweig University of Technology: Braunschweig, DE

1985-09-01 to 1990-11-30 | Dipl.-Ing. (Civil engineering)
Education
Source: Self-asserted source
Richard Degenhardt

Works (50 of 79)

Items per page:
Page 1 of 2

Exact geometric nonlinear analysis of frames modeled with nonprismatic shear-deformable elements defined by noncentroidal axes

Engineering Structures
2025-01 | Journal article
DOI: 10.1016/j.engstruct.2024.119267
Contributors: Francisco C. de Araújo; Protáze Mageveske; Richard Degenhardt
Source: check_circle
Crossref

Shape and loading imperfection sensitivity of the vibration-correlation technique for buckling analysis of cylindrical shells

Engineering Structures
2024-04 | Journal article
DOI: 10.1016/j.engstruct.2024.117605
Contributors: T.D. Baciu; F. Franzoni; R. Degenhardt; K. Kalnins; C. Bisagni
Source: check_circle
Crossref

Sensitivity analysis for buckling characterisation using the vibration correlation technique

Thin-Walled Structures
2023-02 | Journal article
DOI: 10.1016/j.tws.2022.110329
Contributors: Theodor D. Baciu; Richard Degenhardt; Felipe Franzoni; Adrian Gliszczynski; Mariano A. Arbelo; Saullo G.P. Castro; Kaspars Kalnins
Source: check_circle
Crossref

Influence of Spatially Distributed Out-of-Plane CFRP Fiber Waviness on the Estimation of Knock-Down Factors Based on Stochastic Numerical Analysis

Journal of Composites Science
2022-11-22 | Journal article
DOI: 10.3390/jcs6120353
Contributors: Andreas Schuster; Richard Degenhardt; Christian Willberg; Tobias Wille
Source: check_circle
Crossref

Enhanced vibration correlation technique to predict the buckling load of unstiffened composite cylindrical shells

Journal of Sound and Vibration
2022-10 | Journal article
DOI: 10.1016/j.jsv.2022.117280
Contributors: Felipe Franzoni; Adrian Gliszczynski; Theodor Dan Baciu; Mariano Andrés Arbelo; Richard Degenhardt
Source: check_circle
Crossref

Assessing the axial buckling load of a pressurized orthotropic cylindrical shell through vibration correlation technique

Thin-Walled Structures
2019 | Journal article
DOI: 10.1016/j.tws.2019.01.009
EID:

2-s2.0-85060484603
Contributors: Franzoni, F.; Odermann, F.; Wilckens, D.; Skuķis, E.; Kalniņš, K.; Arbelo, M.A.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Experimental validation of the vibration correlation technique robustness to predict buckling of unstiffened composite cylindrical shells

Composite Structures
2019 | Journal article
DOI: 10.1016/j.compstruct.2019.111107
EID:

2-s2.0-85066875204
Contributors: Franzoni, F.; Odermann, F.; Lanbans, E.; Bisagni, C.; Andrés Arbelo, M.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Vibration correlation technique for predicting the buckling load of imperfection-sensitive isotropic cylindrical shells: An analytical and numerical verification

Thin-Walled Structures
2019 | Journal article
DOI: 10.1016/j.tws.2019.03.041
EID:

2-s2.0-85063294775
Contributors: Franzoni, F.; Degenhardt, R.; Albus, J.; Arbelo, M.A.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Analytical, numerical, and experimental predictions for free vibrations and buckling of pressurized orthotropic cylindrical shells

Proceedings of the International Astronautical Congress, IAC
2018 | Conference paper
EID:

2-s2.0-85065341604
Contributors: Franzoni, F.; Albus, J.; Arbelo, M.A.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Guest editorial

Aircraft Engineering and Aerospace Technology
2018 | Journal article
DOI: 10.1108/AEAT-02-2018-0084
EID:

2-s2.0-85045911216
Contributors: Degenhardt, R.; Cohen, L.J.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Buckling of axially compressed CFRP cylinders with and without additional lateral load: Experimental and numerical investigation

Thin-Walled Structures
2017 | Journal article
DOI: 10.1016/j.tws.2017.06.002
EID:

2-s2.0-85020447407
Contributors: Khakimova, R.; Castro, S.G.P.; Wilckens, D.; Rohwer, K.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Introduction

International Journal of Computational Methods in Engineering Science and Mechanics
2017 | Journal article
DOI: 10.1080/15502287.2016.1276335
EID:

2-s2.0-85013403190
Contributors: Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Stability of composite shell-type structures

Stability and Vibrations of Thin-Walled Composite Structures
2017 | Book chapter
Part of DOI: 10.1016/B978-0-08-100410-4.00007-7
EID:

2-s2.0-85054242100
Contributors: Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Stability of composite stringer-stiffened panels

Stability and Vibrations of Thin-Walled Composite Structures
2017 | Book chapter
Part of DOI: 10.1016/B978-0-08-100410-4.00009-0
EID:

2-s2.0-85054238178
Contributors: Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Buckling of axially compressed CFRP truncated cones with additional lateral load: Experimental and numerical investigation

Composite Structures
2016 | Journal article
DOI: 10.1016/j.compstruct.2016.08.011
EID:

2-s2.0-84987984901
Contributors: Khakimova, R.; Zimmermann, R.; Wilckens, D.; Rohwer, K.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Buckling of axially compressed CFRP truncated cones: Experimental and numerical investigation

Composite Structures
2016 | Journal article
DOI: 10.1016/j.compstruct.2016.02.023
EID:

2-s2.0-84962252350
Contributors: Khakimova, R.; Wilckens, D.; Reichardt, J.; Zimmermann, R.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Design and Manufacture of Conical Shell Structures Using Prepreg Laminates

Applied Composite Materials
2016 | Journal article
DOI: 10.1007/s10443-015-9461-4
EID:

2-s2.0-84940557119
Contributors: Khakimova, R.; Burau, F.; Degenhardt, R.; Siebert, M.; Castro, S.G.P.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Investigation on the Geometric Imperfections driven Local Buckling Onset in Composite Conical Shells

Applied Composite Materials
2016 | Journal article
DOI: 10.1007/s10443-016-9490-7
EID:

2-s2.0-84964391062
Contributors: Di Pasqua, M.F.; Khakimova, R.; Castro, S.G.P.; Arbelo, M.A.; Riccio, A.; Raimondo, A.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

New design scenario for future composite launcher structures

30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016
2016 | Conference paper
EID:

2-s2.0-85013636560
Contributors: Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

A semi-analytical approach for linear and non-linear analysis of unstiffened laminated composite cylinders and cones under axial, torsion and pressure loads

Thin-Walled Structures
2015 | Journal article
DOI: 10.1016/j.tws.2015.01.002
EID:

2-s2.0-84921957823
Contributors: Castro, S.G.P.; Mittelstedt, C.; Monteiro, F.A.C.; Arbelo, M.A.; Degenhardt, R.; Ziegmann, G.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Evaluation of non-linear buckling loads of geometrically imperfect composite cylinders and cones with the Ritz method

Composite Structures
2015 | Journal article
DOI: 10.1016/j.compstruct.2014.11.050
EID:

2-s2.0-84919770071
Contributors: Castro, S.G.P.; Mittelstedt, C.; Monteiro, F.A.C.; Degenhardt, R.; Ziegmann, G.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Experimental and numerical estimation of buckling load on unstiffened cylindrical shells using a vibration correlation technique

Thin-Walled Structures
2015 | Journal article
DOI: 10.1016/j.tws.2015.04.024
EID:

2-s2.0-84929155957
Contributors: Arbelo, M.A.; Kalnins, K.; Ozolins, O.; Skukis, E.; Castro, S.G.P.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Experimental nondestructive test for estimation of buckling load on unstiffened cylindrical shells using vibration correlation technique

Shock and Vibration
2015 | Journal article
DOI: 10.1155/2015/729684
EID:

2-s2.0-84940121684
Contributors: Kalnins, K.; Arbelo, M.A.; Ozolins, O.; Skukis, E.; Castro, S.G.P.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Improved stochastic methods for modelling imperfections for buckling analysis of composite cylindrical shells

Engineering Structures
2015 | Journal article
DOI: 10.1016/j.engstruct.2015.06.013
EID:

2-s2.0-84932639892
Contributors: Kepple, J.; Herath, M.; Pearce, G.; Prusty, G.; Thomson, R.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Investigation of Buckling Behavior of Composite Shell Structures with Cutouts

Applied Composite Materials
2015 | Journal article
DOI: 10.1007/s10443-014-9428-x
EID:

2-s2.0-84948581780
Contributors: Arbelo, M.A.; Herrmann, A.; Castro, S.G.P.; Khakimova, R.; Zimmermann, R.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Stochastic analysis of imperfection sensitive unstiffened composite cylinders using realistic imperfection models

Composite Structures
2015 | Journal article
DOI: 10.1016/j.compstruct.2015.02.063
EID:

2-s2.0-84924714864
Contributors: Kepple, J.; Herath, M.T.; Pearce, G.; Gangadhara Prusty, B.; Thomson, R.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

The Influence of Geometrical Parameters on the Buckling Behavior of Conical Shell by the Single Perturbation Load Approach

Applied Composite Materials
2015 | Journal article
DOI: 10.1007/s10443-014-9414-3
EID:

2-s2.0-84938332369
Contributors: Di Pasqua, M.F.; Khakimova, R.; Castro, S.G.P.; Arbelo, M.A.; Riccio, A.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

A robustness-based design strategy for composite structures

Aircraft Engineering and Aerospace Technology
2014 | Journal article
DOI: 10.1108/AEAT-04-2013-0070
EID:

2-s2.0-84918546563
Contributors: Da Cunha, F.R.S.; Wille, T.; Degenhardt, R.; Sinapius, M.; De Araújo, F.C.; Zimmermann, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

A robustness-based design strategy for composite structures - Probabilistic approach

Aircraft Engineering and Aerospace Technology
2014 | Journal article
DOI: 10.1108/AEAT-04-2013-0071
EID:

2-s2.0-84918556992
Contributors: Da Cunha, F.R.S.; Wille, T.; Degenhardt, R.; Sinapius, M.; De Araújo, F.C.; Zimmermann, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Aeroelastic behavior of composite wings in post buckling regime

29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
2014 | Conference paper
EID:

2-s2.0-84910640458
Contributors: De Oliveira, L.C.; Degenhardt, R.; Klimmek, T.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Buckling and postbuckling of truncated conical shells with varying semi-vertex angle: The use of the single perturbation load approach

54th Israel Annual Conference on Aerospace Sciences 2014
2014 | Conference paper
EID:

2-s2.0-84904675826
Contributors: Khakimova, R.; Zimmermann, R.; Di Pascua, M.F.; Castro, S.G.P.; Arbelo, M.A.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Future structural stability design for composite space and airframe structures

Thin-Walled Structures
2014 | Journal article
DOI: 10.1016/j.tws.2014.02.020
EID:

2-s2.0-84900989860
Contributors: Degenhardt, R.; Castro, S.G.P.; Arbelo, M.A.; Zimmerman, R.; Khakimova, R.; Kling, A.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Geometric imperfections and lower-bound methods used to calculate knock-down factors for axially compressed composite cylindrical shells

Thin-Walled Structures
2014 | Journal article
DOI: 10.1016/j.tws.2013.08.011
EID:

2-s2.0-84886502358
Contributors: Castro, S.G.P.; Zimmermann, R.; Arbelo, M.A.; Khakimova, R.; Hilburger, M.W.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Improving the correlation of finite element models using vibration correlation technique on composite cylindrical shells

54th Israel Annual Conference on Aerospace Sciences 2014
2014 | Conference paper
EID:

2-s2.0-84904889764
Contributors: Arbelo, M.A.; Castro, S.G.P.; Khakimova, R.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Linear buckling predictions of unstiffened laminated composite cylinders and cones under various loading and boundary conditions using semi-analytical models

Composite Structures
2014 | Journal article
DOI: 10.1016/j.compstruct.2014.07.037
EID:

2-s2.0-84919711488
Contributors: Castro, S.G.P.; Mittelstedt, C.; Monteiro, F.A.C.; Arbelo, M.A.; Ziegmann, G.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Numerical characterization of imperfection sensitive composite structures

Composite Structures
2014 | Journal article
DOI: 10.1016/j.compstruct.2013.09.041
EID:

2-s2.0-84896983736
Contributors: Arbelo, M.A.; Degenhardt, R.; Castro, S.G.P.; Zimmermann, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Ritz method for the analysis of unstiffened laminated composite cylinders and cones under axial compression

54th Israel Annual Conference on Aerospace Sciences 2014
2014 | Conference paper
EID:

2-s2.0-84904682922
Contributors: Castro, S.G.P.; Mittelstedt, C.; Monteiro, F.A.C.; Arbelo, M.A.; Khakimova, R.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

The single perturbation load approach applied to imperfection sensitive conical composite structures

Thin-Walled Structures
2014 | Journal article
DOI: 10.1016/j.tws.2014.07.005
EID:

2-s2.0-84907320158
Contributors: Khakimova, R.; Warren, C.J.; Zimmermann, R.; Castro, S.G.P.; Arbelo, M.A.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Verification study on buckling behaviour of composite cylinder with eccentric supports

54th Israel Annual Conference on Aerospace Sciences 2014
2014 | Conference paper
EID:

2-s2.0-84904621582
Contributors: Kalnins, K.; Ozoliņš, O.; Arbelo, M.A.; Degenhardt, R.; Castro, S.G.P.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Vibration correlation technique for the estimation of real boundary conditions and buckling load of unstiffened plates and cylindrical shells

Thin-Walled Structures
2014 | Journal article
DOI: 10.1016/j.tws.2014.02.006
EID:

2-s2.0-84896800591
Contributors: Arbelo, M.A.; De Almeida, S.F.M.; Donadon, M.V.; Rett, S.R.; Degenhardt, R.; Castro, S.G.P.; Kalnins, K.; Ozoliņš, O.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

A case study of random field models applied to thin-walled composite cylinders in finite element analysis

Safety, Reliability, Risk and Life-Cycle Performance of Structures and Infrastructures - Proceedings of the 11th International Conference on Structural Safety and Reliability, ICOSSAR 2013
2013 | Conference paper
EID:

2-s2.0-84892397211
Contributors: De Groof, V.; Oberguggenberger, M.; Haller, H.; Degenhardt, R.; Kling, A.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

A SBS-BD based solver for domain decomposition in BE methods

Engineering Analysis with Boundary Elements
2013 | Journal article
DOI: 10.1016/j.enganabound.2013.06.006
EID:

2-s2.0-84880259907
Contributors: De Araújo, F.C.; D'Azevedo, E.F.; Gray, L.J.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Exploring the constancy of the global buckling load after a critical geometric imperfection level in thin-walled cylindrical shells for less conservative knock-down factors

Thin-Walled Structures
2013 | Journal article
DOI: 10.1016/j.tws.2013.06.016
EID:

2-s2.0-84880342507
Contributors: Castro, S.G.P.; Zimmermann, R.; Arbelo, M.A.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Influence of imperfections on axial buckling load of composite cylindrical shells

ICCM International Conferences on Composite Materials
2013 | Conference paper
EID:

2-s2.0-84929342438
Contributors: Kepple, J.; Prusty, B.G.; Pearce, G.; Kelly, D.; Thomson, R.; Degenhardt, R.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Adhesive joints in composite laminates - A combined numerical/experimental estimate of critical energy release rates

International Journal of Adhesion and Adhesives
2012 | Journal article
DOI: 10.1016/j.ijadhadh.2011.09.002
EID:

2-s2.0-81955164861
Contributors: Balzani, C.; Wagner, W.; Wilckens, D.; Degenhardt, R.; Büsing, S.; Reimerdes, H.-G.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Quantitative assessment of random field models in FE buckling analyses of composite cylinders

ECCOMAS 2012 - European Congress on Computational Methods in Applied Sciences and Engineering, e-Book Full Papers
2012 | Conference paper
EID:

2-s2.0-84871625616
Contributors: De Groof, V.; Oberguggenberger, M.; Haller, H.; Degenhardt, R.; Kling, A.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

A study on the robustness of two stiffened composite fuselage panels

Composite Structures
2010 | Journal article
DOI: 10.1016/j.compstruct.2009.07.009
EID:

2-s2.0-70349795523
Contributors: Lee, M.C.W.; Kelly, D.W.; Degenhardt, R.; Thomson, R.S.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Advances in computational stability analysis of composite aerospace structures

AIP Conference Proceedings
2010 | Conference paper
DOI: 10.1063/1.3498128
EID:

2-s2.0-79954565684
Contributors: Degenhardt, R.; De Araújo, F.C.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

An analysis tool for design and certification of postbuckling composite aerospace structures

International Journal of Structural Stability and Dynamics
2010 | Journal article
DOI: 10.1142/S0219455410003671
EID:

2-s2.0-77955704965
Contributors: Orifici, A.C.; Thomson, R.S.; Degenhardt, R.; Bisagni, C.; Bayandor, J.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier

Cyclic buckling tests of pre-damaged CFRP stringer-stiffened panels

International Journal of Structural Stability and Dynamics
2010 | Journal article
DOI: 10.1142/S0219455410003762
EID:

2-s2.0-77955700591
Contributors: Wilckens, D.; Degenhardt, R.; Rohwer, K.; Zimmermann, R.; Kepke, M.; Hildebrandt, B.; Zipfel, A.
Source: Self-asserted source
Richard Degenhardt via Scopus - Elsevier
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Peer review (4 reviews for 2 publications/grants)

Review activity for Archives of Civil and Mechanical Engineering. (1)
Review activity for Composite structures (3)
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