Results 91 to 100 of about 3,713 (199)

Comparative structural evaluation of polymer-based morphing wing ribs using finite element analysis for optimized adaptive aerospace applications

open access: yesJournal of Engineering and Applied Science
Morphing wing ribs are essential for enabling adaptive aerodynamic performance, reduced fuel consumption, and operational flexibility in low-speed aircraft and UAVs. This study presents a comprehensive structural evaluation of trailing-edge morphing ribs
Siddalingappa P Kodigaddi   +2 more
doaj   +1 more source

Development and Experimental Study of a Seamless Morphing Trailing Edge Flap Equipped with an Elephant Trunk Actuation Mechanism

open access: yesApplied Sciences
Following the promising performance of the seamless morphing trailing edge (SMTE) flap and its internal actuation system, the elephant trunk mechanism (ETM), investigated through aerodynamic and structural analyses, this study presents an experimental ...
Mir Hossein Negahban   +2 more
doaj   +1 more source

Design and Numerical Evaluation of Trailing Edge Deflection Distance-Based Morphing Wing

open access: yesEng
This project’s focus is to create a morphing wing with variable geometry that will improve aerodynamic performance. The NACA 0018 airfoil, known for its stable aerodynamic characteristics and symmetrical shape, is chosen as a base airfoil for ...
Periyasamy Sivanandi   +3 more
doaj   +1 more source

Conceptual Design and Analysis of a Trans-Domain Aircraft Based on the Camber Morphing Wing

open access: yesMachines
Multi-functionality and high mission adaptability are important trends in the development of future aircrafts. Trans-domain aircraft, with their unique take-off and landing capabilities and cross-medium capability, have significant potential in the field
Mingzhen Wang   +6 more
doaj   +1 more source

Review of research into shock control bumps [PDF]

open access: yes, 2015
B König   +22 more
core   +2 more sources

Rotational bistable mechanisms for morphing wings and beyond. [PDF]

open access: yesCommun Eng
Barri K   +5 more
europepmc   +1 more source

An aeroacoustic investigation into the effect of self-oscillating trailing edge flaplets [PDF]

open access: yes
The aeroacoustics of a NACA 0012 aerofoil with an array of self-oscillating flexible flaplets attached on the trailing edge has been investigated at low to moderate chord based Reynolds number (50,000 -- 350,000) and at geometric angles of attack from ...
Bruecker, C., Geyer, T. F., Talboys, E.
core  

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