TOWARDS AN ANALYTICAL MODEL FOR FILM COOLING PREDICTION USING INTEGRAL TURBULENT BOUNDARY LAYER

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.

SIKARWAR B.S.; BHADAURIA A.; RANJAN P.

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

Journal Paper

Paper Information

Journal: International Journal of Engineering Year:2016 | Volume:29 | Issue:4 (TRANSACTIONS A: BASICS) Page(s): 554-562

Download Full-Text

View:

299

Download:

261

Cites:

Information Journal Paper

Title

TOWARDS AN ANALYTICAL MODEL FOR FILM COOLING PREDICTION USING INTEGRAL TURBULENT BOUNDARY LAYER

Author(s)

SIKARWAR B.S. | BHADAURIA A. | RANJAN P. | Issue Writer Certificate

Keywords

FILM

COOLING

ANALYTICAL

HEAT TRANSFER

ROCKET

MODEL

Abstract

The objective of this work is to develop deep theoretical methods that are based on the solution of the integral boundary layer equations for investigating FILM COOLING in liquid ROCKET engine. The integral MODEL assumes that heat is transferred from hot free stream gas to the liquid FILM both by convection and radiation. The mass is transferred to the free srteam gas by the well-known blowing process.Downstream of the liquid FILM, the gas effectiveness is obtained by solving boundary layer integral equations. It incorporates a differential MODEL for calorimeter mixing between liquid vapors in the boundary layer with the free stream gas entrained in the boundary layer. Comparisons with existing theoretical and experimental results indicate the FILM coating trends were well predicted by the present integral MODEL proposed by us.

Multimedia

No record.

Cites

No record.

References

No record.

Cite

APA: Copy

SIKARWAR, B.S., BHADAURIA, A., & RANJAN, P.. (2016). TOWARDS AN ANALYTICAL MODEL FOR FILM COOLING PREDICTION USING INTEGRAL TURBULENT BOUNDARY LAYER. INTERNATIONAL JOURNAL OF ENGINEERING, 29(4 (TRANSACTIONS A: BASICS)), 554-562. SID. https://sid.ir/paper/696079/en

Vancouver: Copy

SIKARWAR B.S., BHADAURIA A., RANJAN P.. TOWARDS AN ANALYTICAL MODEL FOR FILM COOLING PREDICTION USING INTEGRAL TURBULENT BOUNDARY LAYER. INTERNATIONAL JOURNAL OF ENGINEERING[Internet]. 2016;29(4 (TRANSACTIONS A: BASICS)):554-562. Available from: https://sid.ir/paper/696079/en

IEEE: Copy

B.S. SIKARWAR, A. BHADAURIA, and P. RANJAN, “TOWARDS AN ANALYTICAL MODEL FOR FILM COOLING PREDICTION USING INTEGRAL TURBULENT BOUNDARY LAYER,” INTERNATIONAL JOURNAL OF ENGINEERING, vol. 29, no. 4 (TRANSACTIONS A: BASICS), pp. 554–562, 2016, [Online]. Available: https://sid.ir/paper/696079/en

Related Journal Papers

No record.

Related Seminar Papers

No record.

Related Plans

No record.

Recommended Workshops