BOUNDARY INTEGRAL EQUATIONS FOR TIME DOMAIN SOLUTION AND REDUCED ORDER MODELING OF THIN WINGS UNSTEADY AERODYNAMICS

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.

MOHAMMADI AMIN M.; GHADIRI B.; HADDADPOUR H.

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

Journal Paper

Paper Information

Journal: JOURNAL OF AERONAUTICAL ENGINEERING (JOAE) Year:2011 | Volume:13 | Issue:1 Page(s): 39-51

Download Full-Text

Persian Verion

View:

886

Download:

Cites:

Information Journal Paper

Title

BOUNDARY INTEGRAL EQUATIONS FOR TIME DOMAIN SOLUTION AND REDUCED ORDER MODELING OF THIN WINGS UNSTEADY AERODYNAMICS

Author(s)

MOHAMMADI AMIN M. | GHADIRI B. | HADDADPOUR H. | Issue Writer Certificate

Keywords

BOUNDARY INTEGRAL EQUATIONSQ2

BOUNDARY ELEMENT METHODQ3

REDUCED ORDER MODELINGQ2

UNSTEADY AERODYNAMICSQ2

THIN WING AERODYNAMICSQ2

Abstract

In this research, thin wings UNSTEADY AERODYNAMICS has been investigated using BOUNDARY INTEGRAL EQUATIONS. The purpose is to develop a proper basis for the extension of BOUNDARY ELEMENT METHOD applicability to some novel lifting configurations with negligible thickness e.g. membrane wings, flapping and morphing wings. For this purpose, conventional aerodynamic BOUNDARY ELEMENT METHOD that can treat only thick bodies has been formulated and modified so it can be used for thin wings too. Moreover, as boundary element system of equations is expressible in eigenvalue problem form, eigenanalysis of unsteady flow over thin wings has been performed and reduced order aerodynamic models have been constructed based on flow eigenmodes. The proposed BOUNDARY ELEMENT METHOD and BEM-based reduced order models have been used for time domain aerodynamic analysis of various airfoils/wings undergoing different unsteady motions and obtained results are in line with analytical relations, experimental data and verified numerical results.

Cites

REDUCED-ORDER MODELING OF UNSTEADY PARTIAL CAVITY FLOWS USING THE BOUNDARY ELEMENT METHOD

References

No record.

Cite

APA: Copy

MOHAMMADI AMIN, M., GHADIRI, B., & HADDADPOUR, H.. (2011). BOUNDARY INTEGRAL EQUATIONS FOR TIME DOMAIN SOLUTION AND REDUCED ORDER MODELING OF THIN WINGS UNSTEADY AERODYNAMICS. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), 13(1), 39-51. SID. https://sid.ir/paper/173112/en

Vancouver: Copy

MOHAMMADI AMIN M., GHADIRI B., HADDADPOUR H.. BOUNDARY INTEGRAL EQUATIONS FOR TIME DOMAIN SOLUTION AND REDUCED ORDER MODELING OF THIN WINGS UNSTEADY AERODYNAMICS. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE)[Internet]. 2011;13(1):39-51. Available from: https://sid.ir/paper/173112/en

IEEE: Copy

M. MOHAMMADI AMIN, B. GHADIRI, and H. HADDADPOUR, “BOUNDARY INTEGRAL EQUATIONS FOR TIME DOMAIN SOLUTION AND REDUCED ORDER MODELING OF THIN WINGS UNSTEADY AERODYNAMICS,” JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), vol. 13, no. 1, pp. 39–51, 2011, [Online]. Available: https://sid.ir/paper/173112/en

Related Journal Papers