Stagnation Pressure Measurement in High Temperature Jet Flow Using Flying Pitot-Probe

Author(s):  
Predrag Lj. Stefanovic ◽  
Simeon N. Oka ◽  
Pavle B. Pavlovic ◽  
J. Jovanovic ◽  
Miodrag Darko Matovic
Author(s):  
K. Funazaki ◽  
T. Endo ◽  
T. Tanuma

The objective of this study is to reduce secondary flow effects in a linear cascade by sucking the working fluid from the endwall. It is widely known that the secondary flow developed in a cascade has a significant impact on the cascade loss or blade erosion in steam turbines. Therefore, a number of studies have been made on the physics of the secondary flow and several devices to control the secondary flow, such as a fence, have been examined. In this study, considering the application to nozzles in gas turbines or steam turbines, the air suction approach is investigated for reducing the secondary flow effects. A suction slit is provided on the lower endwall of the cascade and a flow rate of the sucked air is controlled by adjusting the exit pressure of the slit. The effects of the suction upon the flow nearby the endwall and the secondary flow are observed through several flow visualizing techniques, for example an oil flow method or a tuft method. Furthermore, velocity and stagnation pressure measurement are conducted by a five-hole pressure tube. This clearly demonstrates the vorticity and loss profiles downstream of the cascade with and without the endwall suction.


1998 ◽  
Vol 84 (8) ◽  
pp. 4049-4059 ◽  
Author(s):  
Yuechao Zhao ◽  
William Barvosa-Carter ◽  
Steven D. Theiss ◽  
Salman Mitha ◽  
Michael J. Aziz ◽  
...  

Author(s):  
Merouane Salhi ◽  
Toufik Zebbiche ◽  
Abderrahmane Mehalem

When the stagnation pressure of a perfect gas increases, the specific heat and their ratio do not remain constant anymore and start to vary with this pressure. The gas does not stay perfect. Its state equation change and it becomes for a real gas. In this case, the effects of molecular size and intermolecular attraction forces intervene to correct the state equation, the thermodynamic parameters and the value of Prandtl Meyer function. The aim of this work is developing a new form of Prandtl Meyer function based on those assumptions; and determining the effect of stagnation pressure on this function. With the assumptions that Berthelot’s state equation accounts for molecular size and intermolecular force effects, expressions are developed for analysing the supersonic flow for thermally and calorically imperfect gas lower than the dissociation molecules threshold. The supersonic parameters depend directly on the stagnation parameters of the combustion chamber. The application is for air. A computation of error was made in this case to give a limit of the perfect gas and the high temperature models compared to the real gas model.


2003 ◽  
Vol 29 (6) ◽  
pp. 836-842 ◽  
Author(s):  
Hirokazu Nakamura ◽  
Toshihiko Shakouchi ◽  
Atsushi Kusuda

2022 ◽  
Author(s):  
Marley A. Albright ◽  
Farhan Arafin ◽  
Erik M. Ninnemann ◽  
Jacklyn P. Higgs ◽  
Subith Vasu

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