Results 311 to 320 of about 940,670 (332)
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Stress Analysis for Bonded Layers
Journal of Applied Mechanics, 1974The problem of a line bond between two layers is solved by techniques appropriate to the plane theory of elasticity. Integral transforms are used to reduce the problem to singular integral equations. Numerical results are obtained for the case of identical layers and the numerical scheme of Erdogan and Gupta proved to be effective for this case. Stress-
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Fracture Analysis of Adhesively Bonded Sheets
Journal of Applied Mechanics, 1976The problem of adhesively bonded sheets, one of which is cracked, is formulated by the utilization of integral transform methods. The objective of the investigation is to calculate the stress-intensity factor at the crack tip for the cracked sheets. Results are obtained when the cracked sheet has a single crack and an array of identical, equally spaced,
Keer, L. M., Lin, C. T., Mura, T.
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Short Strong Hydrogen Bonds: A Valence Bond Analysis
The Journal of Physical Chemistry A, 2002Short strong hydrogen bonds are modeled with two resonating bonding structures issued from a valence bond analysis. A formula giving the bond dissociation energy as a function of the difference in proton affinities (ΔPA) is demonstrated. This equation is expanded in Taylor series and compared to similar equations found in the literature.
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Polar Covalent Bonds: An AIM Analysis of S,O Bonds
The Journal of Physical Chemistry A, 2009The electron distribution for S,O bonds in a wide range of molecules is analyzed using Bader's atoms in molecules theory (AIM) and measures of bond order. It is shown that the electron density and other derived parameters at the bond critical point correlate very well with bond length.
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Non-linear analysis of adhesively bonded joints
International Journal of Non-Linear Mechanics, 1988zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Reddy, J. N., Roy, S.
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Trigger bond analysis of nitroaromatic energetic materials using wiberg bond indices
Journal of Computational Chemistry, 2018The identification of trigger bonds, bonds that break to initiate explosive decomposition, using computational methods could help direct the development of novel, “green” and efficient high energy density materials (HEDMs). Comparing bond densities in energetic materials to reference molecules using Wiberg bond indices (WBIs) provides a relative scale ...
Ashley L. Shoaf, Craig A. Bayse
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Predicting Trigger Bonds in Explosive Materials through Wiberg Bond Index Analysis
ChemPhysChem, 2015AbstractUnderstanding the explosive decomposition pathways of high‐energy‐density materials (HEDMs) is important for developing compounds with improved properties. Rapid reaction rates make the detonation mechanisms of HEDMs difficult to understand, so computational tools are used to predict trigger bonds—weak bonds that break, leading to detonation ...
Lenora K, Harper +2 more
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Bond strength analysis of custom base variables in indirect bonding techniques
American Journal of Orthodontics and Dentofacial Orthopedics, 2008Various methods are used to prepare the cured composite-adhesive interface for orthodontic indirect bonding. The intent of this study was to determine the effect on the shear bond strength of the following variables: use of a filled flowable composite resin as an adhesive, light air-abrasion of the cured composite bracket pad, and wetting the cured ...
Michael A, Thompson +2 more
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Natural Fragment Bond Orbital Method for Interfragment Bonding Interaction Analysis
Journal of the American Chemical SocietyA complex chemical system is often examined based on their fragments, so fragment-based analysis is the key to chemical understanding. We report the natural fragment bond orbital (NFBO) method for interfragment bonding interaction analysis, as an extension to the well-known natural bond orbital method.
Yichi Zhang, Fu Kit Sheong, Zhenyang Lin
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Strength Analysis of Adhesively Bonded Repairs
2003The use of fibre reinforced plastics has grown in recent years in aerospace, automotive and marine structures. The maintenance and repair of these structures are always of main concern to the end-users as well as the manufactures. On an aircraft, the need to repair a component can arise from physical damage due to accidental impact, bird strike ...
Soutis, C, Hu, FZ
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