Results 91 to 100 of about 3,713 (199)
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
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
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
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
Flow Control around the UAS-S45 Pitching Airfoil Using a Dynamically Morphing Leading Edge (DMLE): A Numerical Study. [PDF]
Bashir M +4 more
europepmc +1 more source
Research on Design and Control Method of Flexible Wing Ribs with Chordwise Variable Camber. [PDF]
Tao X, Bin L.
europepmc +1 more source
Rotational bistable mechanisms for morphing wings and beyond. [PDF]
Barri K +5 more
europepmc +1 more source
An aeroacoustic investigation into the effect of self-oscillating trailing edge flaplets [PDF]
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
Soft Active Polymers for Biomimetic Shape Morphing Wings. [PDF]
Yuan C, Liu C, Wang Z.
europepmc +1 more source

