Results 141 to 150 of about 142,516 (311)
Use of Truncated Flapped Airfoils for Impingement and Icing Tests of Full-Scale Leading-Edge Sections [PDF]
In an effort to increase the operational range of existing small icing tunnels, the use of truncated airfoil sections has been suggested. With truncated airfoils, large-scale or even full-scale wing-icing-protection systems could be evaluated. Therefore,
vonGlahn, Uwe H.
core +1 more source
EnergiesSmall wind turbines operating in low wind speed regions have not had any significant success. In addition, small wind speed regions occupy a large area of the world, so they represent a potential area for installing small wind turbines in the future.
Le Quang Sang +7 more
doaj +1 more source
Impingement of Water Droplets on NACA 65A004 Airfoil at 0 Deg Angle of Attack [PDF]
The trajectories of water droplets in the air flowing past an NACA 6511004 airfoil at a n angle of attack of 0 deg were determined. The amount of water in droplet form impinging on the airfoil , the area of droplet impingement, and the rate of droplet ...
Brun, Rinaldo J., Vogt, Dorothea E.
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Constant lift rotor for a heavier than air craft [PDF]
, 1979 A rotor blade extended radially from a hub, characterized by an elongated spar and a plurality of axially aligned shells pivotally mounted on the spar is presented.
Stroub, R. H.
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A compressible solution of the Navier-Stokes equations for turbulent flow about an airfoil [PDF]
A compressible time dependent solution of the Navier-Stokes equations including a transition turbulence model is obtained for the isolated airfoil flow field problem. The equations are solved by a consistently split linearized block implicit scheme.
Gibeling, H. J., Shamroth, S. J.
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Investigation of Water Film Dynamics on the Surface of an Airfoil in a High-Speed Flow and Subsequent Ligament Formation and Breakup From the Trailing Edge [PDF]
Safiullah Safiullah +5 more
openalex +1 more source
Airfoil Diffusion: Denoising Diffusion Model For Conditional Airfoil Generation
20 Pages, 6 ...
Graves, Reid, Farimani, Amir Barati
openaire +2 more sources
NASA low- and medium-speed airfoil development [PDF]
The status of NASA low and medium speed airfoil research is discussed. Effects of airfoil thickness-chord ratios varying from 9 percent to 21 percent on the section characteristics for a design lift coefficient of 0.40 are presented for the initial low ...
Beasley, W. D. +2 more
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