Experimental aerodynamic comparison of active camber morphing and trailing-edge flaps
Unlike hinged flaps (for example, ailerons, elevators, and rudders), camber morphing
devices vary camber distribution in a smooth and continuous way, resulting in aerodynamic …
devices vary camber distribution in a smooth and continuous way, resulting in aerodynamic …
[HTML][HTML] Structural design and analysis of an anisotropic, bi-axially morphing skin concept
Morphing skins as structural component in shape adaptive wings are still in their early
development phase, as they need to combine contradicting requirements, such as extreme …
development phase, as they need to combine contradicting requirements, such as extreme …
Effect of active camber morphing on rotor performance and control loads
D Komp, S Kumar, M Hajek, J Rauleder - Aerospace Science and …, 2021 - Elsevier
A computational investigation of a helicopter main rotor with an active-camber morphing
mechanism was conducted to identify the capability to simultaneously save rotor power and …
mechanism was conducted to identify the capability to simultaneously save rotor power and …
Development of an analytical model for the flexural vibration of fish bone active camber structures with truncated, variable thickness partitions
M Nejati, S Shokrollahi, M Cheraghi - Mechanics Based Design of …, 2024 - Taylor & Francis
The need for smooth, gapless mechanisms that offer superior aerodynamic performance has
been the prime mover for a wide range of studies on the morphing concepts from the early …
been the prime mover for a wide range of studies on the morphing concepts from the early …
Time-domain feedforward control for gust response alleviation based on seamless morphing wing
Y Hu, Y Dai, Y Wu, C Yang - AIAA Journal, 2022 - arc.aiaa.org
This paper presents a time-domain feedforward control scheme for alleviating gust response
by using a seamless wing morphing technique. The morphing device is composed of a …
by using a seamless wing morphing technique. The morphing device is composed of a …
Numerical Investigation and Optimization of a Morphing Airfoil Designed for Lower Reynolds Number
A novel concept of morphing airfoils, capable of changing camber and thickness, is
proposed. A variable airfoil shape, defined by six input parameters, is achieved by allowing …
proposed. A variable airfoil shape, defined by six input parameters, is achieved by allowing …
A Review on Fishbone Active Camber Morphing Wing Surfaces
E Özbek, S Ekici, TH Karakoc - … on Unmanned Systems and The Defense …, 2022 - Springer
Morphing wing applications have been used to change various dimensional properties of
aircraft. Various 2D and 3D parameters can be changed on the aircraft's wings, tail surfaces …
aircraft. Various 2D and 3D parameters can be changed on the aircraft's wings, tail surfaces …
SMA blade twist system: from the requirements to the demonstration in relevant environment
In the present work, an overview is provided on the activities performed by CIRA, DLR and
Univ of Bristol to develop and test a morphing system aimed at altering the twist of a blade to …
Univ of Bristol to develop and test a morphing system aimed at altering the twist of a blade to …
Experimental Investigation of a Novel Morphing Wing Design.
JA Pabon, X Gao, J Cai, S Gunasekaran - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
The aerodynamic performance of a novel Fishbone Skin-Actuated-Camber (SAC) morphing
wing design, which actuates its skin to change its effective camber, was studied both …
wing design, which actuates its skin to change its effective camber, was studied both …
High Fidelity Numerical Characterization of NACA 23012 at Re= 300, 000 through a Discontinuous Galerkin LES Solver
P Valvo, A Abbà, G Gibertini - 2024 - preprints.org
The present paper proposes an accurate characterization of a NACA 23012 airfoil at near
stall conditions at a Reynolds number $ Re= 3\cdot 10^ 5$. In light of the unavoidable limits …
stall conditions at a Reynolds number $ Re= 3\cdot 10^ 5$. In light of the unavoidable limits …