safety relief device
continuous output load
configuration tube
accessory gearbox case
ASSR
rotating rectifier assembly
light control panel
global fatigue damage
/Storage
磁不可靠区域
local airflow
act increment
jet air?
Defect Rectified\
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revprot
revtla
regular passage
regularpassage
maskangel
seamless aluminum shell
自动油门电门
overwrapping
自动油门断开电门
motive flow
D check
6se
quadratic equation??
t1
wiring path
Collar lever
Afolts cards
Passback
FINE Turbo
FINE?/Turbo
FINE?/Turbo
fine?/turbo
the film cooling effectiveness
the film cooling effectiveness of blade
The flow field
The flow field and the film cooling effectiveness of blade are simulated using FINETM/Turbo developed by the Numeca Int.,
override button
quick release strap
SMRT
Agreement between the flat plate data and the suction surface data was reasonably good.
oxygen box door
In recent years, a number of experimental studies and numerical simulations were performed for the mixing flow of jet and mainstream and the adiabatic film cooling effectiveness
The effect of rotation on the flow field and the film cooling effectiveness on the pressure side is more apparent than that on the suction side as is shown in the computational and measured results
Results reveal the secondary flow near the blade surface in the wake region behind the jet hole
and the predictions of the three-dimensional velocities were compared with the measured results by Laser-Doppler Velocimetry (LDV)
Numerical simulation of three-dimensional flow field and film cooling effectiveness in film-cooled turbine rotor and stationary turbine cascade were carried out by using the k - ? turbulence model
FILM-COOLED TURBINE