Simulation of Baffle Effects on Sloshing in Model Aircraft Fuel Tank

Q: How can I download an article?

To download an article from SID, first log in to the site, search for the article title, and click on the 'Download Article' option.

Q: How can I download an ISI article?

To download an ISI article on SID, enter the keyword or article title in the search bar, view the relevant results, click on the desired article, and select the 'Download Article' option.

Q: How can I access the SID database?

To access the SID database, visit SID.ir, create an account, and log in to access scientific resources.

Q: Is downloading articles from SID free?

Some articles on SID are available for free, while others require payment. Details are specified on the article's page.

MAHMOODI M.; PIRKANDI J.; Amjadian B.; Noorshad H.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: JOURNAL OF SOLID AND FLUID MECHANICS Year:2019 | Volume:9 | Issue:2 Page(s): 275-287

Download Full-Text

Persian Verion

View:

294

Download:

Cites:

Information Journal Paper

Title

Simulation of Baffle Effects on Sloshing in Model Aircraft Fuel Tank

Author(s)

MAHMOODI M. | PIRKANDI J. | Amjadian B. | Noorshad H. | Issue Writer Certificate

Keywords

VOFQ1

Fuel Tank SloshingQ1

BaffleQ1

Aircraft Fuel SystemQ1

Abstract

One of ways to prevent sloshing in fuel tanks is to use Baffles inside the tanks. In this research, 5 tank samples, including a non-Baffle and Baffle tanks are modeled in 3D. In the following, by applying the gravitational acceleration to the tank, the effects of the Baffle’ s shape on sloshing and fluid motion inside the fuel tank have been analysed by using the numerical method of volume of fluid (VOF), the results indicate an error value of less than 4% between numerical and experimental methods. Based on the results, the fluid sloshing reaches a relative stability after 0. 35 seconds, while in non-Baffle tank, this relative stability occurs after 1. 1 seconds. According to the results, the motion of the fuel is in the position of the Baffle in bottom and middle is higher with respect to the lower height Baffle than the position with the upper Baffle in the tank. Based on the results obtained in the simultaneous positioning of the Baffles in the bottom, middle and upper, the fluid created less sloshing and the fuel pipe is in a better position than the Baffles in other fuel tanks.

Cites

No record.

References

No record.

Cite

APA: Copy

MAHMOODI, M., PIRKANDI, J., Amjadian, B., & Noorshad, H.. (2019). Simulation of Baffle Effects on Sloshing in Model Aircraft Fuel Tank. JOURNAL OF SOLID AND FLUID MECHANICS, 9(2 ), 275-287. SID. https://sid.ir/paper/375816/en

Vancouver: Copy

MAHMOODI M., PIRKANDI J., Amjadian B., Noorshad H.. Simulation of Baffle Effects on Sloshing in Model Aircraft Fuel Tank. JOURNAL OF SOLID AND FLUID MECHANICS[Internet]. 2019;9(2 ):275-287. Available from: https://sid.ir/paper/375816/en

IEEE: Copy

M. MAHMOODI, J. PIRKANDI, B. Amjadian, and H. Noorshad, “Simulation of Baffle Effects on Sloshing in Model Aircraft Fuel Tank,” JOURNAL OF SOLID AND FLUID MECHANICS, vol. 9, no. 2 , pp. 275–287, 2019, [Online]. Available: https://sid.ir/paper/375816/en

Related Journal Papers