RAPID SUBSONIC FLUTTER ANALYSIS FOR LOW ASPECT RATIO COMPOSITE WINGS

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.

BASIRI M.; Farrokhfal H.; MOSAYEBI M.; KOOHI R.

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

Journal Paper

Paper Information

Journal: IRANIAN JOURNAL OF MECHANICAL ENGINEERING (ENGLISH) Year:2022 | Volume:23 | Issue:1 Page(s): 68-86

Download Full-Text

View:

Download:

Cites:

Information Journal Paper

Title

RAPID SUBSONIC FLUTTER ANALYSIS FOR LOW ASPECT RATIO COMPOSITE WINGS

Author(s)

BASIRI M. | Farrokhfal H. | MOSAYEBI M. | KOOHI R. | Issue Writer Certificate

Keywords

Flutter

Equivalent plate

Composite

Doublet point method

Abstract

This study aims to achieve effective analysis and fast modeling in free vibration and Flutter analyses of low aspect ratio Composite wings in subsonic flow for the preliminary design stage instead of using the computationally expensive finite element method. It uses an Equivalent plate method for structural modeling. Also, it uses the doublet point and the U-g methods for calculation of unsteady aerodynamic loads and carrying out Flutter analysis, respectively. We investigate the effects of different parameters on the Flutter behavior. The present results confirm that the structural tailoring can make a harmonious balance to the wing sweep angle effect upon the Flutter behavior of Composite wings, and a considerable improvement upon Flutter performance is achieved by using Composite materials.

Multimedia

No record.

Cites

No record.

References

No record.

Cite

APA: Copy

BASIRI, M., Farrokhfal, H., MOSAYEBI, M., & KOOHI, R.. (2022). RAPID SUBSONIC FLUTTER ANALYSIS FOR LOW ASPECT RATIO COMPOSITE WINGS. IRANIAN JOURNAL OF MECHANICAL ENGINEERING TRANSACTIONS OF THE ISME, 23(1), 68-86. SID. https://sid.ir/paper/1034775/en

Vancouver: Copy

BASIRI M., Farrokhfal H., MOSAYEBI M., KOOHI R.. RAPID SUBSONIC FLUTTER ANALYSIS FOR LOW ASPECT RATIO COMPOSITE WINGS. IRANIAN JOURNAL OF MECHANICAL ENGINEERING TRANSACTIONS OF THE ISME[Internet]. 2022;23(1):68-86. Available from: https://sid.ir/paper/1034775/en

IEEE: Copy

M. BASIRI, H. Farrokhfal, M. MOSAYEBI, and R. KOOHI, “RAPID SUBSONIC FLUTTER ANALYSIS FOR LOW ASPECT RATIO COMPOSITE WINGS,” IRANIAN JOURNAL OF MECHANICAL ENGINEERING TRANSACTIONS OF THE ISME, vol. 23, no. 1, pp. 68–86, 2022, [Online]. Available: https://sid.ir/paper/1034775/en

Related Journal Papers

No record.

Related Seminar Papers

No record.

Related Plans

No record.

Recommended Workshops