Non-contact 3D flow-structure interaction measurement (FSIM) system for motion and flow fields

2006 ◽  
Vol 9 (3) ◽  
pp. 265-274 ◽  
Author(s):  
D. H. Doh ◽  
T. G. Hwang ◽  
H. J. Jo ◽  
Y. B. Pyeon ◽  
Y. B. Cho ◽  
...  
Author(s):  
Tadd T. Truscott ◽  
Jesse Belden ◽  
Joseph R. Nielson ◽  
David J. Daily ◽  
Scott L. Thomson

Author(s):  
Jiří Dobeš ◽  
Jaroslav Fořt ◽  
Jiří Fürst ◽  
Jan Halama ◽  
Karel Kozel

2022 ◽  
Author(s):  
Yoo-Jin Ahn ◽  
Mustafa N. Musta ◽  
Marc A. Eitner ◽  
Jayant Sirohi ◽  
Noel T. Clemens

2019 ◽  
Vol 111 ◽  
pp. 02010
Author(s):  
Nikolay Ivanov ◽  
Marina Zasimova ◽  
Evgueni Smirnov ◽  
Alexey Abramov ◽  
Detelin Markov ◽  
...  

The study is devoted to the Unsteady Reynolds-Averaged Navies-Stokes (URANS) simulation of ventilation in an isothermal room with numerous jets supplied from ceiling diffusers. The computations of the airflow under the test conditions considered were carried out in the classroom of the Technical University of Sofia with no occupants. The room floor has a simple rectangular form, but several columns, beams, window sills, and four radiators are located inside the room that makes the geometry more complex. Air is supplied to the room through four ceiling fan coils, the Reynolds number is 2×104. Calculations were carried out using the ANSYS Fluent 18.2 software with the standard k-ε turbulence model chosen. Computational meshes of up to 33 million hexahedral cells clustered to the inlet and outlet sections were used. The main aim of the study presented is to analyze and discuss the complicated 3D flow structure in the room and to give foundation for future measurements of air velocity field in the room.


2006 ◽  
Vol 39 ◽  
pp. S601 ◽  
Author(s):  
S. Deguchi ◽  
Y. Miyake ◽  
A. Shiota ◽  
Y. Tamura ◽  
S. Washio

Author(s):  
Kozo Fujii ◽  
Akira Oyama ◽  
Nobuyuki Tsuboi ◽  
Moto Tsukada ◽  
Hirofumi Ouchi ◽  
...  

Flow fields of Mach number 2.2 jet impinging on an inclined flat plate are experimentally investigated using the Pressure Sensitive Paints (PSP) and Schlieren flow visualization. The flow filed structure is mainly determined by two geometrical parameters (nozzle-plate distance and plate angle against the jet) and one flow parameter (pressure ratio). The results suggest that all the observed flow fields can actually be classified into three types of flow structure based on the three parameters above. As an extension of the authors’ earlier work, experiments are carried out for higher plate angles. The new results show the effectiveness and limitation of the classification that we proposed. To find out the flow structure, some of the flow fields are computationally simulated. Good agreement of the pressure distributions with the experiment validates the simulation. Although analysis so far is limited, the result reveals three dimensional complex flow structure that created pressure peaks over the plate surface.


Author(s):  
YaoWei Hu ◽  
JiangSheng Wang ◽  
JinJun Wang ◽  
Christian Breitsamter

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