Experimental and numerical failure analysis of thin-walled composite plates using progressive failure analysis
K Falkowicz - Composite Structures, 2023 - Elsevier
This study investigates the stability and failure analysis of thin-walled composite plate
elements weakened by cut-out and subjected to axial compression. Tested plates were …
elements weakened by cut-out and subjected to axial compression. Tested plates were …
Optimal design of plated/shell structures under flutter constraints—A literature review
Aeroelastic optimization has become an indispensable component in the evaluation of
divergence and flutter characteristics for plated/shell structures. The present paper intends to …
divergence and flutter characteristics for plated/shell structures. The present paper intends to …
Buckling analysis of laminated plates with asymmetric layup by approximation method
K Falkowicz, P Wysmulski, H Debski - Materials, 2023 - mdpi.com
This study investigated thin-walled plate elements with a central cut-out under axial
compression. The plates were manufactured from epoxy/carbon laminate (CFRP) with an …
compression. The plates were manufactured from epoxy/carbon laminate (CFRP) with an …
Optimum design of composite structures: A literature survey (1969–2009)
FO Sonmez - Journal of Reinforced Plastics and Composites, 2017 - journals.sagepub.com
Optimum structural design of composites is a research subject that has drawn the attention
of many researchers for more than 40 years with a growing interest. In this study, a review of …
of many researchers for more than 40 years with a growing interest. In this study, a review of …
A novel dynamic aeroelastic framework for aeroelastic tailoring and structural optimisation
NPM Werter, R De Breuker - Composite Structures, 2016 - Elsevier
Driven by a need to improve the efficiency of aircraft and reduce the fuel consumption,
composite materials are applied extensively in the design of aircraft. A dynamic aeroelastic …
composite materials are applied extensively in the design of aircraft. A dynamic aeroelastic …
Impact behavior and damage characteristics of hygrothermally conditioned carbon epoxy composite laminates
A novel finding about effects of moisture and cyclic hygrothermal conditions on the impact
resistance of carbon fiber reinforced epoxy polymer (CFRP) composites are presented. The …
resistance of carbon fiber reinforced epoxy polymer (CFRP) composites are presented. The …
[HTML][HTML] Design and testing of aeroelastically tailored composite wing under fatigue and gust loading including effect of fatigue on aeroelastic performance
D Rajpal, FMA Mitrotta, CA Socci, J Sodja… - Composite …, 2021 - Elsevier
The aim of the paper is to experimentally validate a numerical design methodology for
optimizing composite wings subject to gust and fatigue loading requirements and to assess …
optimizing composite wings subject to gust and fatigue loading requirements and to assess …
Viscous fluid–structure interaction response of composite hydrofoils
Composite materials are increasingly used in hydrodynamic lifting surfaces due to their
higher specific strength and favorable fatigue properties. A set of parametric studies are …
higher specific strength and favorable fatigue properties. A set of parametric studies are …
Structural analysis and optimization of a tethered swept wing for airborne wind energy generation
In this paper, we present an aero‐structural model of a tethered swept wing for airborne
wind energy generation. The carbon composite wing has neither fuselage nor actuated …
wind energy generation. The carbon composite wing has neither fuselage nor actuated …
Aeroelastic tailoring of transport aircraft wings: state-of-the-art and potential enabling technologies
C Jutte, BK Stanford - 2014 - ntrs.nasa.gov
This paper provides a brief overview of the state-of-the-art for aeroelastic tailoring of
subsonic transport aircraft and offers additional resources on related research efforts …
subsonic transport aircraft and offers additional resources on related research efforts …