Experimental Investigations Into Damage Tolerance of Honeycomb Sandwich Panels
Author : Ani Ural
Publisher :
Page : 282 pages
File Size : 40,95 MB
Release : 1999
Category :
ISBN :
Author : Ani Ural
Publisher :
Page : 282 pages
File Size : 40,95 MB
Release : 1999
Category :
ISBN :
Author :
Publisher :
Page : 608 pages
File Size : 27,59 MB
Release : 1985
Category : Astronautics
ISBN :
Author :
Publisher :
Page : 188 pages
File Size : 12,23 MB
Release : 2002
Category : Airframes
ISBN :
The impact responses and the damage states in flat composite sandwich panels with thin face sheets were investigated in Phase I and were found to be dependent on the diameter of the spherical steel impactor. The residual strength of impact-damaged sandwich panels under static in-plane compressive loads was reported to be dependent on the nature of the damage state. The impact damage due to blunt impactors is difficult to detect in service and depending on the size of the damage, can degrade the residual strength more than a punctured skin. The detectability of impact damage states using different field inspection techniques was experimentally investigated for different facesheet and core combinations. The impact damage in honeycomb core sandwich panels was better detected using instruments that exploit the local vibrational characteristics of the sandwich structure, while the damage in foam core panels was more amenable to acoustic-based techniques. The effect of facesheet stiffness on the sensitivity of the field inspection techniques was investigated and the results are reported. The behavior of the sandwich panels with impact damage and subjected to the in-plane static compressive loads was investigated in detail. The impact damage behaved in a characteristic sequence of events leading to contrasting final failure modes. The sequence of events was found to be dependent on the facesheet stiffness and the transverse compressive properties of the core material. The effects of panel curvature on the impact damage resistance of sandwich panels were experimentally investigated for limited sandwich configurations. The effects of the radius of cylindrical panels, boundary conditions, facesheet type, and core type were also examined. The decreasing radius of curvature increased the global bending stiffness but decreased the local contact stiffness due to the radial compressive properties of the honeycomb core.
Author :
Publisher :
Page : 994 pages
File Size : 24,56 MB
Release :
Category : Aeronautics
ISBN :
Author : Serge Abrate
Publisher : Springer Science & Business Media
Page : 646 pages
File Size : 31,89 MB
Release : 2012-11-02
Category : Science
ISBN : 9400753292
This book presents a broad view of the current state of the art regarding the dynamic response of composite and sandwich structures subjected to impacts and explosions. Each chapter combines a thorough assessment of the literature with original contributions made by the authors. The first section deals with fluid-structure interactions in marine structures. The first chapter focuses on hull slamming and particularly cases in which the deformation of the structure affects the motion of the fluid during the water entry of flexible hulls. Chapter 2 presents an extensive series of tests underwater and in the air to determine the effects of explosions on composite and sandwich structures. Full-scale structures were subjected to significant explosive charges, and such results are extremely rare in the open literature. Chapter 3 describes a simple geometrical theory of diffraction for describing the interaction of an underwater blast wave with submerged structures. The second section addresses the problem of impact on laminated composite structures with chapters devoted to ballistic impacts on pre-stressed composite structures, tests developed to simulate dynamic failure in marine structures, damage mechanisms and energy absorption in low velocity impacts, perforation, the numerical simulation of intra and inter-ply damage during impact, and hail impact on laminated composites. Sandwich structures with laminated facings are considered in Section 3 with chapters dealing with the discrete modeling of honeycomb core during the indentation of sandwich structures, the behavior of fold core sandwich structures during impact, and impact on helicopter blades. The fourth section consists of two chapters presenting experimental results and numerical simulation of composite structures subjected to crash. This volume is intended for advanced undergraduate and graduate students, researchers, and engineers interested and involved in analysis and design of composite structures.
Author : Composite Materials Handbook – 17 (CMH-17)
Publisher : SAE International
Page : 353 pages
File Size : 29,3 MB
Release : 2013-09-18
Category : Technology & Engineering
ISBN : 0768080622
The last volume of this six-volume compendium is an update to the cancelled Military Handbook 23, which was prepared for use in the design of structural sandwich polymer composites, primarily for flight vehicles. The information presented includes test methods, material properties, design and analysis techniques, fabrication methods, quality control and inspection procedures, and repair techniques for sandwich structures in military and commercial vehicles. The Composite Materials Handbook, referred to by industry groups as CMH-17, is a six-volume engineering reference tool that contains over 1,000 records of the latest test data for polymer matrix, metal matrix, ceramic matrix, and structural sandwich composites. CMH-17 provides information and guidance necessary to design and fabricate end items from composite materials. It includes properties of composite materials that meet specific data requirements as well as guidelines for design, analysis, material selection, manufacturing, quality control, and repair. The primary purpose of the handbook is to standardize engineering methodologies related to testing, data reduction, and reporting of property data for current and emerging composite materials. It is used by engineers worldwide in designing and fabricating products made from composite materials.
Author :
Publisher :
Page : 934 pages
File Size : 35,32 MB
Release : 1987
Category : Mechanics, Applied
ISBN :
Author : American Society for Composites. Technical Conference
Publisher : CRC Press
Page : 1168 pages
File Size : 45,68 MB
Release : 1993-10-15
Category : Technology & Engineering
ISBN : 9781566761031
Author : Dan Zenkert
Publisher :
Page : 442 pages
File Size : 47,10 MB
Release : 1997
Category : Sandwich construction
ISBN : 9780947817961
Author :
Publisher :
Page : 610 pages
File Size : 17,70 MB
Release : 1995
Category : Aeronautics
ISBN :
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.