Results 31 to 40 of about 2,175,387 (287)

Composite Weak Bosons: a Lattice Analysis

open access: yes, 1994
We present a lattice analysis of a confining Yang-Mills theory without Goldstone boson. We have analytically investigated the model by a strong coupling expansion and by an intensive lattice Monte Carlo simulation using standard lattice QCD methods.
't Hooft   +23 more
core   +1 more source

Reliability analysis and micromechanics: A coupled approach for composite failure prediction [PDF]

open access: yes, 2011
This work aims at associating two classical approaches for the design of composite materials: first, reliability methods that allow to account for the various uncertainties involved in the composite materials behaviour and lead to a rational estimation ...
Dehmous, Hocine, Welemane, Hélène
core   +1 more source

Flutter Characteristics of a Modified Z-Shaped Folding Wing Using a New Non-Intrusive Model

open access: yesAerospace
Unmanned aerial vehicles (UAVs) with folding wings can serve in multiple mission profiles, usually accompanied by sudden changes in flight speed. These bring great challenges to the aeroelastic design of UAVs, especially in the calculation of flutter ...
Wuchao Qi, Shimiao Wu, Sumei Tian
doaj   +1 more source

WAAM-Fabricated Laminated Metal Composites

open access: yesMetals, 2021
Laminated metal composites are a promising design since the hybrid design enables superior and tailorable material properties compared with bulk material.
Niclas Spalek   +3 more
doaj   +1 more source

The Physics of the $\theta$-angle for Composite Extensions of the Standard Model [PDF]

open access: yes, 2013
We analyse the $\theta$-angle physics associated to extensions of the standard model of particle interactions featuring new strongly coupled sectors. We start by providing a pedagogical review of the $\theta$-angle physics for Quantum Chromodynamics (QCD)
Di Vecchia, Paolo, Sannino, Francesco
core   +2 more sources

Two-Stage Assumed Mode Method for Flutter Analysis of Supersonic Panels with Elastic Supports and Attached Masses

open access: yesAerospace
During the service life of a supersonic aircraft, panels are susceptible to damaged boundary supports and unexpected attached masses, which can critically alter their flutter characteristics.
Wuchao Qi, Shuai Yuan, Sumei Tian
doaj   +1 more source

Diboson Signals via Fermi Scale Spin-One States [PDF]

open access: yes, 2015
ATLAS and CMS observe deviations from the expected background in diboson invariant mass searches of new resonances around 2 TeV. We provide a general analysis of the results in terms of spin-one resonances and find that Fermi scale composite dynamics can
Frandsen, Mads T.   +2 more
core   +3 more sources

The HIT Network for Children and Adolescents With CNS Tumors Facilitates Improvements of Diagnostic Assessments, Multimodal Treatments, Individual Counseling, and Research in Germany, Austria, and Switzerland

open access: yesPediatric Blood &Cancer, EarlyView.
ABSTRACT Background The HIT network was established in 2000 to create a population‐based structure aiming to improve survival rates and reduce late effects for children with central nervous system (CNS) tumors by conducting comprehensive clinical trials.
Stefan Rutkowski   +59 more
wiley   +1 more source

Identification of Stable and Drought-Tolerant Soybean Cultivars using AMMI and GGE Biplot Analysis [PDF]

open access: yesپژوهشنامه اصلاح گیاهان زراعی, 2023
Extended Abstract Introduction and Objective:The soybean genotype's stability and high performance are essential factors for long-term development and food security. That the occurrence of various stresses, including drought stress, can cause high losses
Morteza Messhenas   +3 more
doaj  

Symmetric Composite Laminate Stress Analysis [PDF]

open access: yes, 1985
It is demonstrated that COSMIC/NASTRAN may be used to analyze plate and shell structures made of symmetric composite laminates. Although general composite laminates cannot be analyzed using NASTRAN, the theoretical development presented herein indicates ...
Gellin, S., Smolinski, K. F., Wang, T.
core   +1 more source

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