An Ultra-Fast TSP on a CNT Heating Layer for Unsteady Temperature and Heat Flux Measurements in Subsonic Flows. [PDF]
Bitter M +4 more
europepmc +1 more source
HIGH-LIFT BEHAVIOUR OF HALF-MODELS AT FLIGHT REYNOLDS NUMBERS
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]
Diao L +5 more
europepmc +1 more source
Practical Fast-Response Anodized-Aluminum Pressure-Sensitive Paint Using Chemical Adsorption Luminophore as Optical Unsteady Pressure Sensor. [PDF]
Oka Y +5 more
europepmc +1 more source
Numerical Study of Wall Ventilation in a Transonic Wind Tunnel
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
A Generalized Fisher Discriminant Analysis with Adaptive Entropic Regularization for Cross-Model Vibration State Monitoring in Wind Tunnels. [PDF]
Li Z, Li Z, Chen X, Lin H.
europepmc +1 more source
Weak wall boundary conditions for compressible flows. [PDF]
Jaiswal M +4 more
europepmc +1 more source
Three-Dimensional Analysis of Biomimetic Aerofoil in Transonic Flow. [PDF]
Marimuthu S, Al-Rabeei S, Boha HA.
europepmc +1 more source
Three-Dimensional Deformation Calculation of Wind Tunnel Flexible Wall Using Orthogonal Beam Function. [PDF]
Yang X, Ma Y, Wang G, Yang C, Yu C.
europepmc +1 more source
Axial compressor blades tip leakage flow control using natural aspiration. [PDF]
Nejad PG, Zenouz RT.
europepmc +1 more source

