Experimental and numerical study of airflow distribution in an aircraft cabin mock-up with a gasper on

2016 ◽  
Vol 9 (5) ◽  
pp. 555-566 ◽  
Author(s):  
Ruoyu You ◽  
Jun Chen ◽  
Zhu Shi ◽  
Wei Liu ◽  
Chao-Hsin Lin ◽  
...  
2019 ◽  
Vol 85 ◽  
pp. 02015 ◽  
Author(s):  
Charles Berville ◽  
Matei-Răzvan Georgescu ◽  
Ilinca Năstase

The current concept of Crew Quarters on board of the International Space Station has several issues according to the crew member’s feedback. Major issues concern noise levels, the accumulation of CO2 and the quality of the air distribution. Our study targets the airflow distribution, to diagnose this issue, we realise a series of numerical simulations (CFD) based on a real scale replica of the Crew Quarters. Simulations were set with a zero-gravity mode and with the theoretical air parameters inside the SSI. The geometry includes a thermal manikin having the neutral posture of a body in the absence of gravity. Numerical simulations were run for the three different air flow rates provided by the current ventilation system. Results have shown that the air distribution inside the Crew Quarter is insufficient for low airflow rates but becomes acceptable for the higher airflow rate, however the higher airflow rate can potentially produce draught discomfort.


2015 ◽  
Vol 34 (5) ◽  
pp. 595-607 ◽  
Author(s):  
H. Scaar ◽  
G. Franke ◽  
F. Weigler ◽  
M. Delele ◽  
E. Tsotsas ◽  
...  

2021 ◽  
Vol 2111 (1) ◽  
pp. 012012
Author(s):  
A Jamaldi ◽  
Sarjito ◽  
A S Nurrohkayati ◽  
N T Atmoko

Abstract This paper examines the effect of different mesh types on a numerical study of evaporative cooling in the chimney. This research is a follow-up study from previous research. The test specimen used is an evaporative chimney design with the addition of a nozzle arrangement in it. The main focus of this research is the study of mesh refinement, namely by applying structured mesh during the simulation process. Three types of mesh with different levels of fineness were used for the specimens. They are coarse ( mesh A), medium (mesh B), and fine (mesh C). In addition to differences in mesh, research was also carried out with variations in the level of relative humidity (RH). The RH levels used are 5, 10, and 15%. Two main parameters of evaporative cooling performance are airflow distribution and temperature drop in the chimney. Method for measuring the distribution of airflow and temperature drop in the chimney by making five planes with different heights. The results showed that the simulation with mesh B produced a good agreement data with previous studies than mesh A and C. The RH level that generated the most optimal cooling is found at 5% RH.


2011 ◽  
Vol 312-315 ◽  
pp. 865-870 ◽  
Author(s):  
M.B. Acikgoz ◽  
Baris Akay ◽  
Antonio F. Miguel ◽  
Murat Aydın

Airborne pathogens can spread within an aircraft cabin from sneezing, coughing or breathing of a sick passenger. This paper reports a 3D numerical study on the transport of airborne pathogens inside Boeing 767 cabin. After cough or sneeze of an infected passenger, the entire unsteady pathogen dispersion process is simulated. Effects under study include the direction of coughing on the pathogens propagation and the spreading times from infected to hosts passengers.


2011 ◽  
Vol 48 (6) ◽  
pp. 1994-2001 ◽  
Author(s):  
Chaofan Wu ◽  
Noor A. Ahmed

2018 ◽  
Vol 140 ◽  
pp. 128-139 ◽  
Author(s):  
Xiaolei Yuan ◽  
Yu Wang ◽  
Jinxiang Liu ◽  
Xinjie Xu ◽  
Xiaohang Yuan

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