Results 61 to 70 of about 23,423 (133)

Combined genetic algorithm and response surface methodology‐based bi‐optimization of a vertical‐axis wind turbine numerically simulated using CFD

open access: yesEnergy Science &Engineering, Volume 12, Issue 10, Page 4532-4548, October 2024.
The optimum values of moment and lift force for a vertical axis wind turbine were determined by a multi‐objective optimization methodology including response surface methodology (RSM), computational fluid dynamic (CFD), Non‐Dominated Sorting Genetic Algorithm (NSGA‐II), and the Technique for Order of Preference by Similarity to Ideal Solution (TOPSIS).
Mahdi Roshani   +2 more
wiley   +1 more source

A Naturally Inspired Extrusion‐Based Microfluidic Approach for Manufacturing Tailorable Magnetic Soft Continuum Microrobotic Devices

open access: yesAdvanced Materials, Volume 36, Issue 31, August 1, 2024.
Here, microfluidics is leveraged to precisely control reaction‐diffusion (RD) processes for generating multifunctional and compartmentalized alginate‐based microfibers. This nature‐inspired RD process allows for producing sophisticated fibers acting as magnetic soft continuum robots.
Lukas Hertle   +13 more
wiley   +1 more source

NUMERICAL INVESTIGATION OF TWO ELEMENT CAMBER MORPHING AIRFOIL IN LOW REYNOLDS NUMBER FLOWS [PDF]

open access: yesJournal of Engineering Science and Technology, 2017
Aerodynamic performance of a two-element camber morphing airfoil was investigated at low Reynolds number using the transient SST model in ANSYS FLUENT 14.0 and eN method in XFLR5. The two-element camber morphing concept was employed to morph the baseline
RAJESH SENTHIL KUMAR T.   +3 more
doaj  

Aerodynamic design of a double slotted morphed flap airfoil– a numerical study

open access: yesFrontiers in Mechanical Engineering
Introduction:The objective of this study is to develop and simulate a double slotted morphed flap with the intention of reducing drag and enhancing lift, thereby leading to a smaller flap size and reduced weight.Methods:A flap was meticulously designed ...
S. S. Shahrokhi   +2 more
doaj   +1 more source

Knowledge-Based Shape Optimization of Morphing Wing for More Efficient Aircraft

open access: yesInternational Journal of Aerospace Engineering, 2015
An optimization procedure for the shape design of morphing aircraft is presented. The process is coupled with a knowledge-based framework combining parametric geometry representation, multidisciplinary modelling, and genetic algorithm.
Alessandro De Gaspari, Sergio Ricci
doaj   +1 more source

Aerodynamic optimisation of a camber morphing aerofoil [PDF]

open access: yes, 2015
An aircraft that has been carefully optimised for a single flight condition will tend to perform poorly at other flight conditions. For aircraft such as long-haul airliners, this is not necessarily a problem, since the cruise condition so heavily ...
Fincham, J.H.S.   +2 more
core   +1 more source

An Experimental and Simulation Study of the Active Camber Morphing Concept on Airfoils Using Bio-Inspired Structures. [PDF]

open access: yesBiomimetics (Basel), 2023
Dharmdas A   +8 more
europepmc   +1 more source

Design & modelling of a composite rudderless aeroelastic fin structure [PDF]

open access: yes, 2010
This thesis presents the study of a gapless and rudderless aeroelastic fin (GRAF) to enhance the directional stability and controllability of an aircraft. The GRAF concept was proposed and developed in the wake of previous research, targeted to improve
Trapani, Matteo
core   +3 more sources

Construction of a Morphing Wing Rib Actuated by a NiTi Wire

open access: yesJournal of Aerospace Technology and Management, 2015
The main goal of this paper is to analyze if it is feasible to employ a trained shape memory alloy wire as a linear actuator to modify the camber of a morphing wing rib.
Thais Campos de Almeida   +2 more
doaj  

High-Bandwidth Morphing Actuator for Aeroelastic Model Control

open access: yesAerospace, 2019
The design and testing of a high-bandwidth continuous actuator for aeronautical applications is presented hereinafter. The actuator has a dual goal of controlling both the aeroelastic behaviour and the flight mechanics of the model in which it is ...
Sebastiano Fichera   +2 more
doaj   +1 more source

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