2017
DOI: 10.1177/0954410016684360
|View full text |Cite
|
Sign up to set email alerts
|

Vibration analysis of a rotating variable thickness bladed disk for aircraft gas turbine engine using generalized differential quadrature method

Abstract: In this paper, free vibration analysis of rotating variable thickness annular bladed disk suitable to be used in aircraft gas turbine engine is investigated. The numerical generalized differential quadrature method is introduced in this paper as a fast and efficient numerical method to be used for vibration analysis of bladed disks of real gas turbine engines. The boundary conditions are supposed to be similar to those of the real bladed disk used in the aircraft engines i.e. clamped for the inner edge and fre… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
5

Citation Types

0
6
0

Year Published

2017
2017
2024
2024

Publication Types

Select...
9
1

Relationship

0
10

Authors

Journals

citations
Cited by 11 publications
(6 citation statements)
references
References 22 publications
0
6
0
Order By: Relevance
“…The GDQ method is an improvement of the DQ method, especially for solving higher order di erential equations, which is more computationally e cient and accurate. Unlike the DQ method, the GDQ method considers a general situation, where the derivatives of a function are approximated using a linear weighted sum of all the functional values and also some derivatives of the functional values [23,24]. From the above discussion on the previous papers in the literature and to the best of the authors' knowledge, the vibration analysis of rotating functionally graded thin disk with variable thickness has not been investigated so far.…”
Section: Introductionmentioning
confidence: 95%
“…The GDQ method is an improvement of the DQ method, especially for solving higher order di erential equations, which is more computationally e cient and accurate. Unlike the DQ method, the GDQ method considers a general situation, where the derivatives of a function are approximated using a linear weighted sum of all the functional values and also some derivatives of the functional values [23,24]. From the above discussion on the previous papers in the literature and to the best of the authors' knowledge, the vibration analysis of rotating functionally graded thin disk with variable thickness has not been investigated so far.…”
Section: Introductionmentioning
confidence: 95%
“…2,[7][8][9][10][11] In addition, the dynamic performance was considered in many studies. [12][13][14] Furthermore, numerous researchers referred to the stark impacts of the materials' temperature dependency on the performance. 11,15 Some of the above studies considered structures (disc/cylinder) made of homogeneous materials that are usually metals.…”
Section: Introductionmentioning
confidence: 99%
“…They used finite difference method to find the stresses and displacements. Shahriari et al [15] applied differential quadrature method to investigate the vibration of rotating bladed disk used in gas turbine engines. They considered the disk to be flexible with the same material as the real gas turbine disk and the blades of the bladed disks to be rigid.…”
Section: Introductionmentioning
confidence: 99%