Results 121 to 130 of about 49,450 (147)

Data-Driven Sparse Sensor Placement Optimization on Wings for Flight-By-Feel: Bioinspired Approach and Application. [PDF]

Biomimetics (Basel)
Hollenbeck AC, Beachy AJ, Grandhi RV, Pankonien AM.   +3 more
europepmc   +1 more source

Effect of Coupled Wing Motion on the Aerodynamic Performance during Different Flight Stages of Pigeon. [PDF]

Cyborg Bionic Syst
Shen Y, Xu Y, Huang W, Shang C, Shi Q.
europepmc   +1 more source

Agile manoeuvrable flight via collaborative wing-tail adjustment of a flapping wing robot. [PDF]

Commun Eng
Liu G, Pan E, Sun W, Wang S, Xu W, Yan L.   +5 more
europepmc   +1 more source

Neural fields for rapid aircraft aerodynamics simulations. [PDF]

Sci Rep
Catalani G, Agarwal S, Bertrand X, Tost F, Bauerheim M, Morlier J.   +5 more
europepmc   +1 more source

New Leading-Edge Reinforcement Design of Aircraft Wing to Withstand Bird Collision. [PDF]

Biomimetics (Basel)
Ngamlikitlert S, Kim M, Sleesongsom S.
europepmc   +1 more source

<i>Microraptor</i> reveals specialized gliding capabilities in multiwinged early paravians. [PDF]

Proc Natl Acad Sci U S A
Hefler C, Wang Y, Wang X, Zheng X, Kaye TG, Grosmougin M, Chotard M, Barlow L, Qiu H, Dececchi TA, Habib MB, Shyy W, Pittman M.   +12 more
europepmc   +1 more source

Design, Dynamics and Development of Upgraded Tiltable Wing associated Quadcopter through Advanced computational simulations incorporated Bottom-Up Approach. [PDF]

Sci Rep
Saravana Mohan H, Murugaraj K, Solaiappan SK, Stanislaus Arputharaj B, Rajendran P, Lee IE, Jayakumar SS, Veeraperumal Senthil Nathan JP, Karuppasamy A, Raja V.   +9 more
europepmc   +1 more source

Electrothermally controlled origami fabricated by 4D printing of continuous fiber-reinforced composites. [PDF]

Nat Commun
Wang Y, Ye H, He J, Ge Q, Xiong Y.
europepmc   +1 more source

Hierarchical modeling and optimization of camber morphing airfoil

Aerospace Science and Technology, 2015
A variable camber morphing airfoil with compliant ribs and flexible composite skins is studied in a hierarchical modeling framework. The key requirements of a variable camber morphing airfoil are the flexible skin, compliant internal structure and a ...
Senthil Murugan, M I Friswell
exaly   +2 more sources

Concepts for morphing airfoil sections using bi-stable laminated composite structures

Thin-Walled Structures, 2008
The present paper investigates the potential of using bi-stable laminated composite structures for morphing an airfoil section. The objective of the paper is to identify geometries and lay-ups of candidate configurations that offer multiple stable shapes
Paul Weaver
exaly   +2 more sources