The Influence of Axial Compression on the Free Vibration Frequencies of Cross-ply Laminated and Moderately Thick Cylinders

Cagdas, Izzet U.

doi:10.2339/politeknik.447210

Cited by 1 publication

(2 citation statements)

References 22 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…Putting equation ( 11 ) in equation( 10) becomes (12) The aerodynamic stiffness matrices [Ka] is asymmetric.…”

Section: 1flutter Equation Of Panelmentioning

confidence: 99%

See 1 more Smart Citation

Panel Flutter Numerical Study of Thin Isotropic Flat Plates and Curved Plates with Various Edge Boundary Conditions

Pany

2023

Politeknik Dergisi

View full text Add to dashboard Cite

In this article, supersonic panel flutter analysis of flat plates and curved plates with different edge boundary conditions are studied, using efficient, high precision triangular shallow shell finite elements. The fluid on the underside of the plate was is assumed to be stationary. The linear piston theory can be applied to the top surface of the plate. The linear piston theory was used to evaluate the aerodynamic loads. The solution of a complex eigenvalue problem was formulated according to Hamilton’s principle. Lagrange’s equation of motion was obtained using standard methods for finding eigenvalues. Current finite element analysis ignores aerodynamic damping. For panels, the theory of thin and small deformed shells was taken into account. To validate the developed finite element code, the results of a square and rectangular flat-panels with simply supported edges (S-S-S-S), a square plate with four fixed edges (C-C-C-C), and a square plate with the length side clamps (C-S-C-S) were compared with the published data. The flutter results of other edge boundary conditions (S-C-S-C, C-S-C-S, and C-C-C-C) for square and rectangular flat panels are evaluated for which literature data is limited. It has been found that the fixed condition in the cross-flow direction (S-C-S-C) has a significant effect on the critical flutter pressure parameters and flutter frequencies. Further, to study the aforementioned effect, the current finite element (FE) has been extended to curved plates with S-C-S-C(constrained in the cross-flow direction and exposed to supersonic flow), SS-S-S boundary conditions to find flutter results.

show abstract

“…Putting equation ( 11 ) in equation( 10) becomes (12) The aerodynamic stiffness matrices [Ka] is asymmetric.…”

Section: 1flutter Equation Of Panelmentioning

confidence: 99%

“…Long, thick-walled composite cylinders with internally or externally pressurized fixed ends have been investigated [10]. The free vibrational behaviour of axially compressed cross-laminated composite cylinders has been studied using FSDT-based shell FEs with various boundary conditions [11].…”

Section: Introductionmentioning

confidence: 99%

Panel Flutter Numerical Study of Thin Isotropic Flat Plates and Curved Plates with Various Edge Boundary Conditions

Pany

2023

Politeknik Dergisi

View full text Add to dashboard Cite

show abstract

The Influence of Axial Compression on the Free Vibration Frequencies of Cross-ply Laminated and Moderately Thick Cylinders

Cited by 1 publication

References 22 publications

Panel Flutter Numerical Study of Thin Isotropic Flat Plates and Curved Plates with Various Edge Boundary Conditions

Panel Flutter Numerical Study of Thin Isotropic Flat Plates and Curved Plates with Various Edge Boundary Conditions

Contact Info

Product

Resources

About