Results 71 to 80 of about 5,264 (176)
Aerodynamic performance analysis of a little penguin wing and penguin‐inspired wing is numerically conducted at a chord‐based Reynolds number Re = 105 to assess its feasibility for use in microair vehicles (MAVs). The results strongly suggest that penguin‐inspired wing shape performs in a superior manner at higher angles of attack (AOAs) in comparison ...
Mahadi Hasan Masud +4 more
wiley +1 more source
IGA-based Multi-Index Stochastic Collocation for random PDEs on arbitrary domains
This paper proposes an extension of the Multi-Index Stochastic Collocation (MISC) method for forward uncertainty quantification (UQ) problems in computational domains of shape other than a square or cube, by exploiting isogeometric analysis (IGA ...
Beck, Joakim +2 more
core +1 more source
Constant‐Ratio Blended Models of Curves and Surfaces in Euclidean 3‐Space
We consider a simple blending method for parametric curves and surfaces. The described blending method offers a systematic approach to creating smooth transitions between parametric curves and surfaces while maintaining Cn‐continuity. It utilizes the parametrizations of the original objects to achieve predictable variations in shape and enables the ...
B. Bulca Sokur, Mohammad W. Alomari
wiley +1 more source
Novel freeform optical design methods can be classified in two categories, depending on whether they focus on the generation of a starting point or the development of new optimization tools.
Clément Freslier +10 more
doaj +1 more source
In this work, we have combined the template method with the mapping method to innovate a four‐step mesh generation method for planar geometric models. This method enables the rapid generation of high‐quality, density‐controllable quadrilateral meshes.
Yize Li, Qingyuan Hu, Gengdong Cheng
wiley +1 more source
In this paper, we implement the finite detail technique primarily based on T-Splines for approximating solutions to the linear elasticity equations in the connected and bounded Lipschitz domain.
Said EL Fakkoussi +4 more
doaj +1 more source
Parameterized Modeling of Blended Wing Body Aircraft Based on Multi-Scale CST Method [PDF]
In the parameterized modeling of blended wing body aircraft, the commonly used CST method has weak local deformation control capability, while the Non-Uniform Rational B-Splines(NURBS)method has the problem of too many global parameters.
Wang Kangjun, Wang Wenkai, Zheng Xiaolin
doaj +1 more source
Numerical simulation of individualized flow diversion cerebral aneurysms treatment
Abstract Flow diverter implantation has emerged as a highly effective treatment for cerebral aneurysms. However, the variability in patient‐specific vascular anatomy necessitates detailed pre‐operative planning to mitigate potential complications arising from standard, one‐size‐fits‐all devices. To address these challenges, robust predictive simulation
Huy Quang Do +3 more
wiley +1 more source
Isogeometric Analysis (IGA) has been applied to heterogeneous reactor physics problems using the multigroup neutron dif- fusion equation. IGA uses a computer-aided design (CAD) description of the geometry commonly built from Non-Uniform Rational B ...
Eaton, M, Kophazi, J, Owens, A, Welch, J
core +2 more sources
The continuous adjoint method for transitional flows of compressible fluids was developed and assessed in aerodynamic shape optimization problems, based on three variants of the γ−R˜eθt$$ \gamma -\tilde{R}{e}_{\theta t} $$ transition model. The differentiation of the transition model ensures the accurate computation of the sensitivity derivatives when ...
Marina G. Kontou +3 more
wiley +1 more source

