Results 31 to 40 of about 748 (184)
Experimental Aerodynamic Comparison of Active Camber Morphing and Trailing-Edge Flaps [PDF]
Unlike hinged flaps (for example, ailerons, elevators, and rudders), camber morphing devices vary camber distribution in a smooth and continuous way, resulting in aerodynamic efficiency improvements due to the absence of sharp changes in airfoil camber.
Rivero, Andres E. +4 more
openaire +6 more sources
Design and Experiment of a Seamless Morphing Trailing Edge
Morphing trailing edge wing as an important morphing wing technology has gained wide attention because of its advantages, such as gust mitigation, improved aerodynamic efficiency, and reduced radar reflective area.
Gui Cheng +4 more
doaj +1 more source
Aerodynamic and aeroacoustic characteristics of a bionic morphing flap
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
Structure design of variable camber wing trailing edge based on multi-block rotating mechanism
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
Geometrically nonlinear electro-aeroelastic framework for morphing wing with piezoelectric actuators
In this paper, a flexible morphing wing with piezoelectric materials for morphing actuation is studied. The objectives of this paper are 1) to develop an integrated geometrically nonlinear electro-aeroelastic framework, which allows evaluating ...
Natsuki TSUSHIMA +3 more
doaj +1 more source
In-situ boundary layer transition detection on multi-segmental (a)synchronous morphing wings
This paper presents an experimental method to detect in-situ the location of transition on a multi-segmental trailing edge camber morphing wing during synchronous and asynchronous morphing.
Vincent L. Stuber +3 more
doaj +1 more source
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
Study on Flow Mechanism of a Morphing Supercritical Airfoil
In order to maintain the best performance in flight, a new concept, morphing aircraft, has been proposed, which can change the real-time aerodynamic characteristics under different flight conditions.
Yuanjing Wang +4 more
doaj +1 more source
Study on the Actuation Aspects for a Morphing Aileron Using an Energy–Based Design Approach
Evaluating the impact of morphing devices in terms of actuation energy is a promising approach to quantify, from the earliest stages of wing design, the convenience of active camber morphing compared to the use of conventional control surfaces.
Alessandro De Gaspari
doaj +1 more source
The presented aircraft is capable of alternating between two singular working points by folding the exterior surfaces of the wing underneath the interior surfaces. This allows for a significant change in wingspan, lift surfaces, aspect ratio and airfoil (
Amit Geva, Haim Abramovich, Rimon Arieli
doaj +1 more source

