NUMERICAL AND EXPERIMENTAL INVESTIGATION ON THE EFFECT OF A PLASMA ACTUATOR ON NLF0414 AIRFOILS' EFFICIENCY AFTER THE STALL

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.

SALMASI A.; SHADARAM A.; MIRZAEI M.; SHAMS TALEGHANI A.

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

Journal Paper

Paper Information

Journal: Modares Mechanical Engineering Year:2013 | Volume:12 | Issue:6 Page(s): 104-116

Download Full-Text

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

Persian Verion

View:

1,104

Download:

Cites:

Information Journal Paper

Title

NUMERICAL AND EXPERIMENTAL INVESTIGATION ON THE EFFECT OF A PLASMA ACTUATOR ON NLF0414 AIRFOILS' EFFICIENCY AFTER THE STALL

Author(s)

SALMASI A. | SHADARAM A. | MIRZAEI M. | SHAMS TALEGHANI A. | Issue Writer Certificate

Keywords

PLASMA ACTUATORQ2

ACTIVE FLOW CONTROL METHODQ2

SEPARATION POINTQ3

STALL ANGELQ2

Abstract

PLASMA ACTUATOR is one of the newest devices in flow control techniques which can delay separation by inducing external momentum to the boundary layer of the flow. The purpose of this paper is to simulate a NLF0414 airfoil both experimentally and numerically in presence of the body force vector induced by a specific PLASMA ACTUATOR. For this reason, the simulation is done both numerically and experimentally for a NLF0414 airfoil with the compressible 25m/s velocity airflow in two different cases: with no PLASMA ACTUATOR located on the airfoil and with body force produced by a PLASMA ACTUATOR located on the top of the airfoil in order to investigate the effect of plasma on the flow passing over it. The results showed that presence of a PLASMA ACTUATOR on the top surface of the airfoil, close to the SEPARATION POINT, transferred the SEPARATION POINT from x=16 mm to x=41 mm at the angle of attack of 18 degrees. This separation delay caused a 35% increase in the ratio of lift to drag coefficient or the efficiency of the airfoil in the same angle of attack.

Cites

No record.

References

No record.

Cite

APA: Copy

SALMASI, A., SHADARAM, A., MIRZAEI, M., & SHAMS TALEGHANI, A.. (2013). NUMERICAL AND EXPERIMENTAL INVESTIGATION ON THE EFFECT OF A PLASMA ACTUATOR ON NLF0414 AIRFOILS' EFFICIENCY AFTER THE STALL. MODARES MECHANICAL ENGINEERING, 12(6), 104-116. SID. https://sid.ir/paper/178586/en

Vancouver: Copy

SALMASI A., SHADARAM A., MIRZAEI M., SHAMS TALEGHANI A.. NUMERICAL AND EXPERIMENTAL INVESTIGATION ON THE EFFECT OF A PLASMA ACTUATOR ON NLF0414 AIRFOILS' EFFICIENCY AFTER THE STALL. MODARES MECHANICAL ENGINEERING[Internet]. 2013;12(6):104-116. Available from: https://sid.ir/paper/178586/en

IEEE: Copy

A. SALMASI, A. SHADARAM, M. MIRZAEI, and A. SHAMS TALEGHANI, “NUMERICAL AND EXPERIMENTAL INVESTIGATION ON THE EFFECT OF A PLASMA ACTUATOR ON NLF0414 AIRFOILS' EFFICIENCY AFTER THE STALL,” MODARES MECHANICAL ENGINEERING, vol. 12, no. 6, pp. 104–116, 2013, [Online]. Available: https://sid.ir/paper/178586/en

Related Journal Papers