Results 271 to 280 of about 106,651 (339)

Simulation of aircraft flights with turbulence and icing conditions. [PDF]

Sci Data
Dampeyrou C, Ghienne M, Tschannen V, Dion JL.   +3 more
europepmc   +1 more source

Design and Validation of a Biomimetic Leg-Claw Mechanism Capable of Perching and Grasping for Multirotor Drones. [PDF]

Biomimetics (Basel)
Zhao Y, Xiang R, Li H, Wang C, Zhang J, Liu X, Hao Y.   +6 more
europepmc   +1 more source

Long-duration spaceflight adversely affects astronaut piloting performance. [PDF]

Sci Rep
Moore ST, Sims TR, Dilda V, MacDougall HG.   +3 more
europepmc   +1 more source

A physiologically inspired hybrid CPG/Reflex controller for cycling simulations that generalizes to walking. [PDF]

PLoS Comput Biol
Severini G, Muñoz D.
europepmc   +1 more source

Shimmy in a nonlinear model of an aircraft nose landing gear with non-zero rake angle [PDF]

, 2008
Krauskopf, B, Lowenberg, MH, Thota, P
core  

Pot losses and associated implications in Barents sea snow crab fishery. [PDF]

Sci Rep
Cerbule K, Larsen RB, Rijkure A.
europepmc   +1 more source

The Structural Design and Optimization of a Novel Independently Driven Bionic Ornithopter. [PDF]

Biomimetics (Basel)
Dai M, Wu R, Ye M, Gao K, Chen B, Tao X, Fan Z.   +6 more
europepmc   +1 more source

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Further Noise Reduction of Regional Jet Two-Wheel Main Landing Gear

Journal of Aircraft, 2022
Noise reduction design concepts have been applied to a regional jet’s two-wheel main landing gear to reduce airframe noise during the approach. Several concepts were initially developed for the main landing gear of the Japan Aerospace Exploration Agency ...
Yasushi Ito, T. Takaishi, Hirokazu Shoji, Akihisa Shimada, Kensuke Hayashi, Yosuke Ueno   +5 more
semanticscholar   +2 more sources

Failure analysis of aircraft main landing gear cylinder support

Engineering Failure Analysis, 2021
Abstract The main concern in aircraft structures is flight safety. One of the constraints to consider when designing safe aircraft parts is weight. The design of the landing gear structures is difficult because it must ensure flight safety without adding excessive weight. During takeoff, the main landing gear of a cargo plane did not retract.
S. F. Diltemiz
semanticscholar   +2 more sources

Crashworthiness study of UCAV’s main landing gear using explicit dynamics

International Journal of Crashworthiness, 2022
In the aircraft industry, the ultimate goal in any component’s design is to minimize its weight, maximize its durability, and increasing its life while keeping its overall life cycle costs low.
R. F. Swati, Muhammad AsfandYar Amjad, M. Talha, H. Elahi, H. R. Hamdani, A. A. Khan, S. Qureshi   +6 more
semanticscholar   +2 more sources