Results 181 to 190 of about 1,279 (239)

PPO-Based Reinforcement Learning Control of a Flapping-Wing Robot with a Bio-Inspired Sensing and Actuation Feather Unit. [PDF]

Sensors (Basel)
Hussain S, Messaoudi M, Imran M, Tang D.
europepmc   +1 more source

Fuzzy logic based nonlinear blending hybrid control of a kestrel-inspired ornithopter operating in sinusoidal and dryden gusts. [PDF]

Sci Rep
Abbasi SH, Saudagar AKJ, Nouman A, Hennache ML.   +3 more
europepmc   +1 more source

Intelligent computing and sensitivity analysis of unsteady darcy-forchheimer nanofluid flow over an inclined permeable disk subject to thompson-troian slip conditions. [PDF]

Discov Nano
Aldhafeeri AA, Raizah Z, Yasmin H, Algehyne EA.   +3 more
europepmc   +1 more source

Aerodynamic Instability Mechanisms of Iced Eight-Bundled Conductors: Frequency-Domain Analysis and Stability Assessment via Wind Tunnel-CFD Synergy. [PDF]

Sensors (Basel)
Zhong B, Qiao M, Cai M, Hu M.
europepmc   +1 more source

Kinematic and aerodynamic modeling of flexible wings with wing root adjustment for flapping wing micro aerial vehicles. [PDF]

Sci Rep
Liu Z, Zhang X, Wang Z, Ye R.
europepmc   +1 more source

Advanced blade profiles for improved efficiency in Savonius wind turbines: the aeroleaf case study. [PDF]

Sci Rep
Hosseinian SM, Mohseni M, Karimi MS.
europepmc   +1 more source

Numerical investigation of co-flow jet integration to enhance the aerodynamic efficiency of airfoils used in wind turbine applications. [PDF]

Sci Rep
Farghaly MB, El Kader OMA, Alsharif AMA, Halawa M.   +3 more
europepmc   +1 more source

H2 controller design for a kestrel-inspired ornithopter operating in extreme weather. [PDF]

PLoS One
Abbasi SH, Saudagar AKJ, Abbasi N.
europepmc   +1 more source

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On the convergence of unsteady generalized aerodynamic forces

Dynamics Specialists Conference, 1981
Generalized aerodynamic forces computed from analyses based on distributed pressures and finite paneling procedures are examined for solution convergence The necessity for examining the convergence of calculated forces as a function of the number of assumed pressure terms or the number of panels is well demonstrated The lifting series method converges ...
William S. Rowe, Herbert J. Cunningham
openaire   +1 more source

Control of Unsteady Aerodynamic Forces

1990
Abstract : The aerodynamic properties of an airfoil under unsteady conditions are very different from ones in steady conditions because the vortex generated by unsteady separation greatly modifies the loading on the wing. In this study, a fundamental approach was taken to investigate the lift and the velocity field of unsteady airfoils.
Mario Lee, Hank Lin, Chiang Shih, Ismet Gursul, Chih-Ming Ho   +4 more
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