Results 31 to 40 of about 862 (246)

Design and Validation of a New Morphing Camber System by Testing in the Price—Païdoussis Subsonic Wind Tunnel

open access: yesAerospace, 2020
This paper presents the design and wind tunnel testing of a morphing camber system and an estimation of performances on an unmanned aerial vehicle. The morphing camber system is a combination of two subsystems: the morphing trailing edge and the morphing
David Communier   +2 more
doaj   +1 more source

Design and Analysis of MataMorph-3: A Fully Morphing UAV with Camber-Morphing Wings and Tail Stabilizers

open access: yesAerospace, 2022
Conventional aircraft use discrete flight control surfaces to maneuver during flight. The gaps and discontinuities of these control surfaces generate drag, which degrades aerodynamic and power efficiencies.
Peter L. Bishay   +10 more
doaj   +1 more source

Aerodynamic and aeroacoustic characteristics of a bionic morphing flap

open access: yesEnergy Reports, 2023
Birds adapt to the changing flight conditions by performing intricate feather-movements to manipulate the airflow. The avian wings often undergo seamless transformations at the trailing-edge to achieve camber-reflexes for extended flight envelope.
Md. Zishan Akhter   +2 more
doaj   +1 more source

Aerodynamic and Aeroacoustic Performance of Airfoils Fitted with Morphing Trailing-edges [PDF]

open access: yes2018 AIAA/CEAS Aeroacoustics Conference, 2018
Experimental and numerical studies of a simple NACA 0012 airfoil fitted with two different flap profiles were successfully carried out to characterize their aerodynamic and aeroacoustic performance. The airfoil was tested with two flap configurations with different flap camber and a flap deflection angle of = 10.
Kamliya Jawahar, Hasan   +2 more
openaire   +2 more sources

Effects of Trailing Edge Deflections Driven by Shape Memory Alloy Actuators on the Transonic Aerodynamic Characteristics of a Super Critical Airfoil

open access: yesActuators, 2021
A smart structure to actuate a morphing trailing edge based on the super critical airfoil NASA sc-0714(2) was designed and verified in a transonic wind tunnel.
Binbin Lv, Yuanjing Wang, Pengxuan Lei
doaj   +1 more source

Structure design of variable camber wing trailing edge based on multi-block rotating mechanism

open access: yesXibei Gongye Daxue Xuebao, 2023
The variable camber trailing edge enables the aircraft to maintain the best aerodynamic performance throughout the flight envelope, so as to achieve the ultimate goal of reducing aircraft fuel consumption and air pollutant emissions.
SHI Xintong   +4 more
doaj   +1 more source

Adjoint-based optimization of flapping plates hinged with a trailing-edge flap

open access: yesTheoretical and Applied Mechanics Letters, 2015
It is important to understand the impact of wing-morphing on aerodynamic performance in the study of flapping-wing flight of birds and insects. We use a flapping plate hinged with a trailing-edge flap as a simplified model for flexible/morphing wings in ...
Min Xu   +3 more
doaj   +1 more source

Kriging Aerodynamic Modeling and Multi-Objective Control Allocation for Flying Wing UAVs With Morphing Trailing-Edge

open access: yesIEEE Access, 2021
Flexible skin and continuous deformable control surface are the basic of adaptive wing technology for future aircraft. This paper presents a continuous morphing trailing-edge and its control allocation method for the flying wing Unmanned Aerial Vehicle ...
Xinhui Zhao, Yanping Yang, Xiaoping Ma
doaj   +1 more source

Topology Optimization of Large-Scale 3D Morphing Wing Structures

open access: yesActuators, 2021
This work proposes a systematic topology optimization approach for simultaneously designing the morphing functionality and actuation in three-dimensional wing structures.
Peter Dørffler Ladegaard Jensen   +3 more
doaj   +1 more source

Effects of an Unsteady Morphing Wing with Seamless Side-Edge Transition on Aerodynamic Performance

open access: yesEnergies, 2022
This paper presents an unsteady flow analysis of a 3D wing with a morphing trailing edge flap (TEF) and a seamless side-edge transition between the morphed and static parts of a wing by introducing an unsteady parametrization method.
Chawki Abdessemed   +2 more
doaj   +1 more source

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