EXPERIMENTAL DETERMINATION OF THE SUITABLE RANG OF INJECTORS USED IN THE VORTEX COMBUSTION CHAMBER IN LIQUID ROCKET ENGINE

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.

VALIZADEH ESMAEIL; MOUSAVI NAINIYAN SEYED MOJTABA

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

Journal Paper

Paper Information

Journal: AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL Year:2017 | Volume:6 | Issue:1 Page(s): 25-39

Download Full-Text

Persian Verion

View:

838

Download:

Cites:

Information Journal Paper

Title

EXPERIMENTAL DETERMINATION OF THE SUITABLE RANG OF INJECTORS USED IN THE VORTEX COMBUSTION CHAMBER IN LIQUID ROCKET ENGINE

Author(s)

VALIZADEH ESMAEIL | MOUSAVI NAINIYAN SEYED MOJTABA | Issue Writer Certificate

Keywords

COMBUSTION CHAMBER OF LIQUID PROPELLANT ENGINEQ1

VORTEX COMBUSTION CHAMBERQ1

SWIRL INJECTORQ1

OPERATION RANGEQ1

EXPERIMENTAL METHODQ2

Abstract

Vortex combustion chamber which is a new generation of liquid fuel engine with different arrangements of injectors generated a vortex flow into the combustion chamber. This vortex contributed to increased cooling and mixing the components of the propellant in the combustion chamber and can be generated a complete combustion in a small volume chamber. In this chamber several type of injector used in various locations including, centrifugal, flow and vortex injectors. In this study, the design of these injectors and then experimental test to investigate the effect of geometrical parameters on their hydrodynamic characteristics is done using water flow. Spry forming process, flow measurement, pressure drop and injector spray angle including hydrodynamic characteristics that have been studied. The results show acceptable agreement of the predicted design with performance of injectors. Accordingly, centrifugal and flow injectors that injected the fuel and oxidizer into the chamber were selected and shown that increasing the number of tangential vortex injectors to 6, generated more uniformity in the rising vortex flow in the chamber but the entry angle to 5 degrees no significant effect on rising flow.

Cites

No record.

References

No record.

Cite

APA: Copy

VALIZADEH, ESMAEIL, & MOUSAVI NAINIYAN, SEYED MOJTABA. (2017). EXPERIMENTAL DETERMINATION OF THE SUITABLE RANG OF INJECTORS USED IN THE VORTEX COMBUSTION CHAMBER IN LIQUID ROCKET ENGINE. AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL, 6(1 ), 25-39. SID. https://sid.ir/paper/264149/en

Vancouver: Copy

VALIZADEH ESMAEIL, MOUSAVI NAINIYAN SEYED MOJTABA. EXPERIMENTAL DETERMINATION OF THE SUITABLE RANG OF INJECTORS USED IN THE VORTEX COMBUSTION CHAMBER IN LIQUID ROCKET ENGINE. AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL[Internet]. 2017;6(1 ):25-39. Available from: https://sid.ir/paper/264149/en

IEEE: Copy

ESMAEIL VALIZADEH, and SEYED MOJTABA MOUSAVI NAINIYAN, “EXPERIMENTAL DETERMINATION OF THE SUITABLE RANG OF INJECTORS USED IN THE VORTEX COMBUSTION CHAMBER IN LIQUID ROCKET ENGINE,” AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL, vol. 6, no. 1 , pp. 25–39, 2017, [Online]. Available: https://sid.ir/paper/264149/en

Related Journal Papers