Numerical modeling of flow control in a boundary-layer-ingesting offset inlet diffuser at transonic
mach numbers, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada.
The motivation of this study is to generate the training data efficiently for a range of flight parameters including mean angle of attack and Mach number in a transonic
The Spalart-Allmaras turbulence model, which is highly efficient and suitable for the 3D flow with strong pressure gradient, moderate curvature, and separating flows such as transonic
compressor internal flow [11, 23], is adopted to take the turbulence effects into account.
[2.] Saddoughi, S., Bennett, G., Boespflug, M., Puterbaugh, S.L., and Wadia, A.R., 2014, "Experimental Investigation of Tip Clearance Flow in a Transonic
Compressor with and without Plasma Actuators", GT2014-25294, Proc.
Se llevaron a cabo 14 sesiones de hemodialisis con cada uno de los dispositivos recogiendose en todos los casos las presiones arteriales y venosas, el dolor producido por los diferentes dispositivos, los tiempos de hemostasia y los flujos de acceso (QT) a traves del monitor Transonic
The Tricomi equation  is the second-order linear partial differential equations of mixed type, which had been applied to describe the theory of plane transonic
The Tricomi equation was used to describe the transonic
Two of the rounds were borderline transonic
at 1,120 and 1,125 fps.
The James Webb Space Telescope due for launch in 2018 as the successor to the venerable Hubble telescope has to endure the noise and vibration of the 145 dB interaction between rocket engines and launchpad, the jarring transonic
climb phase, the pyroshock as stages separate, turbulent boundary layer excitation, and more.
With the release of the FY2012 DOT&E report, which recommended reducing formance requirements, especially transonic
acceleration and sustained g-forces, the F35 Joint Strike Fighter became another victim in the world of failed aircrafts.
The operating Mach number is usually less than 0.8 for a subsonic cascade, but can go up to 2.0 and more at the tip of a transonic
, for the shock waves in a transonic
region, compression rate is independent of the Reynolds number.