DESIGN AND THEORETICAL - EXPERIMENTAL ANALYSIS OF A FLEXURE PIVOT FOR A PROPULSION SYSTEM TEST STAND

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.

MOKHTARI ALI REZA; MOSAYEBI MASOUD; YOUSEFI SHAHRAM

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:5 | Issue:2 Page(s): 79-91

Download Full-Text

Persian Verion

View:

880

Download:

Cites:

Information Journal Paper

Title

DESIGN AND THEORETICAL - EXPERIMENTAL ANALYSIS OF A FLEXURE PIVOT FOR A PROPULSION SYSTEM TEST STAND

Author(s)

MOKHTARI ALI REZA | MOSAYEBI MASOUD | YOUSEFI SHAHRAM | Issue Writer Certificate

Keywords

FLEXUREQ1

OPTIMIZATION DESIGNQ2

TEST STANDQ1

Abstract

By arrangement of FLEXURE-load cell columns in the six-component TEST STANDs, the thrust vector components of force and moment of a propulsion system can be measured. In this research, the main considerations in the FLEXURE design process of a six component TEST STAND is introduced. Also, a FLEXURE with new geometric structure to take account of these considerations is proposed. Then, by using computational constrained multi-dimensional optimization of direct methods, geometrical dimensions of the FLEXURE are calculated. In the next step, finite element analysis is carried out on designed FLEXURE and its results are compared with results of the analytical solution. To validate the results of the theoretical solution, natural frequencies of the FLEXURE and buckling critical loads are measured experimentally. Based on the acceptable correlation of the theoretical and experimental results, it can be said that the proposed FLEXURE is a good choice for using in a propulsion system six - component TEST STAND.

Cites

No record.

References

No record.

Cite

APA: Copy

MOKHTARI, ALI REZA, MOSAYEBI, MASOUD, & YOUSEFI, SHAHRAM. (2017). DESIGN AND THEORETICAL - EXPERIMENTAL ANALYSIS OF A FLEXURE PIVOT FOR A PROPULSION SYSTEM TEST STAND. AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL, 5(2 ), 79-91. SID. https://sid.ir/paper/264188/en

Vancouver: Copy

MOKHTARI ALI REZA, MOSAYEBI MASOUD, YOUSEFI SHAHRAM. DESIGN AND THEORETICAL - EXPERIMENTAL ANALYSIS OF A FLEXURE PIVOT FOR A PROPULSION SYSTEM TEST STAND. AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL[Internet]. 2017;5(2 ):79-91. Available from: https://sid.ir/paper/264188/en

IEEE: Copy

ALI REZA MOKHTARI, MASOUD MOSAYEBI, and SHAHRAM YOUSEFI, “DESIGN AND THEORETICAL - EXPERIMENTAL ANALYSIS OF A FLEXURE PIVOT FOR A PROPULSION SYSTEM TEST STAND,” AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL, vol. 5, no. 2 , pp. 79–91, 2017, [Online]. Available: https://sid.ir/paper/264188/en

Related Journal Papers