EXPERIMENTAL INVESTIGATION OF ASYMMETRY OF VORTEX FLOW OVER SINGLE DELTA 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.

ATASHBAZ G.

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

Journal Paper

Paper Information

Journal: Journal of Aerospace Science and Technology Year:2004 | Volume:1 | Issue:1 Page(s): 31-39

Download Full-Text

View:

268

Download:

100

Cites:

Information Journal Paper

Title

EXPERIMENTAL INVESTIGATION OF ASYMMETRY OF VORTEX FLOW OVER SINGLE DELTA WINGS

Author(s)

ATASHBAZ G. | Issue Writer Certificate

Keywords

Not Registered.

Abstract

It is generally believed that, on slender delta wings, there is a critical state at which strong asymmetric vortices are found along the leading edge on the leeside of the delta wing. These asymmetric vortices can lead to high lateral forces even when slender delta wing is at the zero angle of yaw. Some experimental studies reported recently, cast considerable doubt as to the validity of the above explanations. A wind tunnel investigation was, therefore, performed to study afresh this phenomenon. The flow over four sharp edged delta wings with aspect to a ratio ranging of 0.56 to 1.46 was investigated using flow visualization with laser light sheet and some surface pressure as well as hot wire measurement. The tests were conducted for angles of attack ranging from 0 to 30 deg and at a free-stream velocity of 30m/s corresponding to a Reynolds number of 4.8 × 105 based on the center line chord of the wing. The results obtained suggest the absence of asymmetry in the vortex core position in the flow.

Multimedia

No record.

Cites

No record.

References

No record.

Cite

APA: Copy

ATASHBAZ, G.. (2004). EXPERIMENTAL INVESTIGATION OF ASYMMETRY OF VORTEX FLOW OVER SINGLE DELTA WINGS. JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST), 1(1), 31-39. SID. https://sid.ir/paper/290916/en

Vancouver: Copy

ATASHBAZ G.. EXPERIMENTAL INVESTIGATION OF ASYMMETRY OF VORTEX FLOW OVER SINGLE DELTA WINGS. JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST)[Internet]. 2004;1(1):31-39. Available from: https://sid.ir/paper/290916/en

IEEE: Copy

G. ATASHBAZ, “EXPERIMENTAL INVESTIGATION OF ASYMMETRY OF VORTEX FLOW OVER SINGLE DELTA WINGS,” JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST), vol. 1, no. 1, pp. 31–39, 2004, [Online]. Available: https://sid.ir/paper/290916/en

Related Journal Papers

No record.

Related Seminar Papers

No record.

Related Plans

No record.

Recommended Workshops