Results 91 to 100 of about 331 (194)

HIGH-LIFT BEHAVIOUR OF HALF-MODELS AT FLIGHT REYNOLDS NUMBERS

open access: yesTASK Quarterly, 2006
A peniche is designed to offset a half-span aircraft model from the wind tunnel wall boundary layer. This strategy of model mounting results in large influence on the measured aerodynamic coefficients, compared with full-span data.
PIOTR DOERFFER, OSKAR SZULC
doaj  

Effect of tip winglet position on tip flow and noise of axial flow fan. [PDF]

open access: yesHeliyon, 2023
Diao L   +5 more
europepmc   +1 more source

Numerical Study of Wall Ventilation in a Transonic Wind Tunnel

open access: yesJournal of Aerospace Technology and Management, 2015
Transonic wind tunnels (TWT) are sophisticated tools for the investigations of flows with Mach numbers of order one. The most characteristic feature of a facility such as this is, for sure, the openings in the walls of the test section.
Bruno Goffert   +2 more
doaj  

Weak wall boundary conditions for compressible flows. [PDF]

open access: yesEng Comput
Jaiswal M   +4 more
europepmc   +1 more source

Three-Dimensional Analysis of Biomimetic Aerofoil in Transonic Flow. [PDF]

open access: yesBiomimetics (Basel), 2022
Marimuthu S, Al-Rabeei S, Boha HA.
europepmc   +1 more source

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