NUMERICAL SIMULATION OF AXISYMMETRIC SUPERSONIC VISCOUS FLOW OVER BLUNT CONE BY USING IMPLICIT FOURTH ORDER FINITE DIFFERENCE METHOD

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.

RASHIDI M.M.; MORADI BASTANI M.

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

Journal Paper

Paper Information

Journal: JOURNAL OF MECHANICAL ENGINEERING AMIRKABIR (AMIRKABIR) Year:2010 | Volume:42 | Issue:2 Page(s): 57-67

Download Full-Text

Persian Verion

View:

1,090

Download:

Cites:

Information Journal Paper

Title

NUMERICAL SIMULATION OF AXISYMMETRIC SUPERSONIC VISCOUS FLOW OVER BLUNT CONE BY USING IMPLICIT FOURTH ORDER FINITE DIFFERENCE METHOD

Author(s)

RASHIDI M.M. | MORADI BASTANI M. | Issue Writer Certificate

Keywords

TLNS EQUATIONSQ3

FOURTH ORDER METHODQ3

SUPERSONIC VISCOUS FLOWQ3

SHOCK-FITTINGQ3

Abstract

In this paper, by using implicit fourth order central difference method and TLNS EQUATIONS, the numerical solution of the steady axisymmetric viscous supersonic flow is implemented over blunt cone with SHOCK-FITTING method. Because of using high order terms of Taylor series in discretization of derivatives, this method has high accuracy and low numerical error (dispersion error) compared with low order method. The boundary-closure scheme has an important role in stability of this method. By using a coarse grid in this method, the results of numerical solution are found to be very close to those obtained with a fine grid employing the second order (Beam-Warming) method. Higher accuracy of this method is identified relative to the second order method when the grid is being refined. The convergence of this method can be adjusted to accommodate the computational hardware capabilities.

Cites

No record.

References

No record.

Cite

APA: Copy

RASHIDI, M.M., & MORADI BASTANI, M.. (2010). NUMERICAL SIMULATION OF AXISYMMETRIC SUPERSONIC VISCOUS FLOW OVER BLUNT CONE BY USING IMPLICIT FOURTH ORDER FINITE DIFFERENCE METHOD. JOURNAL OF MECHANICAL ENGINEERING AMIRKABIR (AMIRKABIR), 42(2), 57-67. SID. https://sid.ir/paper/166000/en

Vancouver: Copy

RASHIDI M.M., MORADI BASTANI M.. NUMERICAL SIMULATION OF AXISYMMETRIC SUPERSONIC VISCOUS FLOW OVER BLUNT CONE BY USING IMPLICIT FOURTH ORDER FINITE DIFFERENCE METHOD. JOURNAL OF MECHANICAL ENGINEERING AMIRKABIR (AMIRKABIR)[Internet]. 2010;42(2):57-67. Available from: https://sid.ir/paper/166000/en

IEEE: Copy

M.M. RASHIDI, and M. MORADI BASTANI, “NUMERICAL SIMULATION OF AXISYMMETRIC SUPERSONIC VISCOUS FLOW OVER BLUNT CONE BY USING IMPLICIT FOURTH ORDER FINITE DIFFERENCE METHOD,” JOURNAL OF MECHANICAL ENGINEERING AMIRKABIR (AMIRKABIR), vol. 42, no. 2, pp. 57–67, 2010, [Online]. Available: https://sid.ir/paper/166000/en

Related Journal Papers