Abstract: In the search for new physics beyond the Standard
Model, Flavour Changing Neutral Current (FCNC) is a good research
field in terms of the observability at future colliders. Increased
Higgs production with higher energy and luminosity in colliders
is essential for verification or falsification of our knowledge of
physics and predictions, and the search for new physics. Prospective
electron-proton collider constituent of the Future Circular Collider
project is FCC-eh. It offers great sensitivity due to its high luminosity
and low interference. In this work, thq FCNC interaction vertex
with off-shell top quark decay at electron-proton colliders is studied.
By using MadGraph5_aMC@NLO multi-purpose event generator,
observability of tuh and tch couplings are obtained with equal
coupling scenario. Upper limit on branching ratio of tree level top
quark FCNC decay is determined as 0.012% at FCC-eh with 1 ab ^−1
luminosity.
Abstract: We study the anomalous WWγ and WWZ couplings by
calculating total cross sections of two processes at the LHeC with
electron beam energy Ee=140 GeV and the proton beam energy Ep=7
TeV, and at the FCC-ep collider with the polarized electron beam
energy Ee=80 GeV and the proton beam energy Ep=50 TeV. At the
LHeC with electron beam polarization, we obtain the results for the
difference of upper and lower bounds as (0.975, 0.118) and (0.285,
0.009) for the anomalous (Δκγ, λγ) and (Δκz, λz) couplings,
respectively. As for FCC-ep collider, these bounds are obtained as
(1.101, 0.065) and (0.320, 0.002) at an integrated luminosity of
Lint=100 fb^-1.
Abstract: In this study, the contact problem of a layered composite which consists of two materials with different elastic constants and heights resting on two rigid flat supports with sharp edges is considered. The effect of gravity is neglected. While friction between the layers is taken into account, it is assumed that there is no friction between the supports and the layered composite so that only compressive tractions can be transmitted across the interface. The layered composite is subjected to a uniform clamping pressure over a finite portion of its top surface. The problem is reduced to a singular integral equation in which the contact pressure is the unknown function. The singular integral equation is evaluated numerically and the results for various dimensionless quantities are presented in graphical forms.