Results 61 to 70 of about 49,450 (147)

Study of efficient fluid-structure interaction analysis for morphing wing with corrugated structures

open access: yesNihon Kikai Gakkai ronbunshu, 2019
Morphing wings, which control the flight by changing their own shapes, have attracted much attention by their potential for improving aerodynamic performance. Corrugated structures, which have flexibility in the corrugation direction and high rigidity in
Kensuke SONEDA   +2 more
doaj   +1 more source

Morphing airfoils analysis using dynamic meshing [PDF]

open access: yes, 2018
© 2018, Emerald Publishing Limited. Purpose: The purpose of this paper is to use dynamic meshing to perform CFD analyses of a NACA 0012 airfoil fitted with a morphing trailing edge (TE) flap when it undergoes static and time-dependent morphing.
Yao, Yufeng   +7 more
core   +1 more source

Morphing Skin: Foams

open access: yes, 2022
S.207-230A morphing skin was developed for adaptive wings with multifinger ribs architecture enabling conformal and differential airfoil camber morphing. The skin consists of aluminum profiles for spanwise stability and low temperature elastomer foam and
Nagel, C., Schorsch, O., Lühring, A.
core   +1 more source

The effect of twist morphing on aerodynamic performance of finite wing at low Reynolds number [PDF]

open access: yesEPJ Web of Conferences
This study experimentally investigates the effect of twist morphing on the aerodynamic characteristics of a finite wing at low Reynolds numbers (Re). As the base model, a NACA 0018 airfoil with an aspect ratio of 4 is used.
Gunes Yasemin B.   +4 more
doaj   +1 more source

Development of a New Span-Morphing Wing Core Design

open access: yesDesigns, 2019
This paper presents a new design for the core of a span-morphing unmanned aerial vehicle (UAV) wing that increases the spanwise length of the wing by fifty percent.
Peter L. Bishay   +4 more
doaj   +1 more source

Modeling and control of a morphing airfoil structure [PDF]

open access: yes, 2003
The aeroelastic modeling and robust control design for a morphing airfoil concept is presented. A finite dimensional linear time invariant aeroelastic model was developed for a multi-input, multi-output morphing airfoil structure.
Whitmer, Christopher
core   +1 more source

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

An Additively Manufactured Self-Recovering Morphing Airfoil with Shape Memory Alloy Actuation

open access: yesActuators
Morphing aerospace structures have attracted increasing attention as an efficient solution for improving aerodynamic efficiency by enabling continuous variation of wing geometry under different flight conditions.
Miriam Battaglia, Aniello Riccio
doaj   +1 more source

Improvement of Aerodynamic Performance of Bilaterally Symmetrical Airfoil by Co-Flow Jet and Adaptive Morphing Technology

open access: yesAerospace
For a special bilaterally symmetric airfoil (BSA), this paper designs an active flow control scheme based on the Co-Flow Jet (CFJ) and adaptive morphing technology, and establishes a numerical simulation method which is suitable for simulating ...
Zeyu Lu, Hongming Cai
doaj   +1 more source

A Preliminary Evaluation of Morphing Horizontal Tail Design for UAVs

open access: yesAerospace
Morphing structures are a relatively new aircraft technology currently being investigated for a variety of applications, from civil to military. Despite the lack of literature maturity and its complexity, morphing wings offer significant aerodynamic ...
Fernando Montano   +2 more
doaj   +1 more source

Home - About - Disclaimer - Privacy