Results 81 to 90 of about 3,255 (122)

Aerodynamics, sensing and control of insect-scale flapping-wing flight. [PDF]

open access: yesProc Math Phys Eng Sci, 2016
Shyy W   +4 more
europepmc   +1 more source

A program to compute three-dimensional subsonic unsteady aerodynamic characteristics using the doublet lattic method, L216 (DUBFLX). Volume 1: Engineering and usage [PDF]

open access: yes
The program input presented consists of configuration geometry, aerodynamic parameters, and modal data; output includes element geometry, pressure difference distributions, integrated aerodynamic coefficients, stability derivatives, generalized ...
Harrison, B. A., Richard, M.
core   +1 more source

The surprising dynamics of a chain on a pulley: lift off and snapping. [PDF]

open access: yesProc Math Phys Eng Sci, 2016
Brun PT, Audoly B, Goriely A, Vella D.
europepmc   +1 more source

Prediction of unsteady aerodynamic loadings caused by leading edge and trailing edge control surface motions in subsonic compressible flow: Computer program description [PDF]

open access: yes
A digital computer program has been developed to calculate unsteady loadings caused by motions of lifting surfaces with leading edge or trailing edge controls based on the subsonic kernel function approach.
Redman, M. C., Rowe, W. S.
core   +1 more source

Power of the wingbeat: modelling the effects of flapping wings in vertebrate flight. [PDF]

open access: yesProc Math Phys Eng Sci, 2015
Heerenbrink MK   +2 more
europepmc   +1 more source

IPR 2021. [PDF]

open access: yesPediatr Radiol, 2021
europepmc   +1 more source

The back squat: A proposed assessment of functional deficits and technical factors that limit performance. [PDF]

open access: yesStrength Cond J, 2014
Myer GD   +9 more
europepmc   +1 more source

Flight of the dragonflies and damselflies. [PDF]

open access: yesPhilos Trans R Soc Lond B Biol Sci, 2016
Bomphrey RJ   +3 more
europepmc   +1 more source

Main Abstracts. [PDF]

open access: yesEur Stroke J, 2021
europepmc   +1 more source

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