Structural stability of functionally graded panels subjected to aero-thermal loads
By K.-J. Sohn, Ji-Hwan Kim. 2008
114 citations recorded by the source corpus.
Subfields: Civil and Structural Engineering, Control and Systems Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/b0d9028096c3f80286f571ea4b7a4aaaeac0adb8
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Civil and Structural Engineering
- Abdelouahed Tounsi
- Mohammed Sid Ahmed Houari
- K. Swaminathan
- E. A. Adda Bedia
- Erasmo Carrera
- Stéphane P.A. Bordas
- M. Bourada
- Ashraf M. Zenkour
In Control and Systems Engineering
- Mohammed Sid Ahmed Houari
- Abdelouahed Tounsi
- E. A. Adda Bedia
- M. Bourada
- Octavio Andrés González-Estrada
- Sundararajan Natarajan
- Erasmo Carrera
- M. Bachir Bouiadjra
In Mechanics of Materials
- Abdelouahed Tounsi
- Mohammed Sid Ahmed Houari
- K. Swaminathan
- E. A. Adda Bedia
- Stéphane P.A. Bordas
- Hung Nguyen-Xuan
- Timon Rabczuk
- Erasmo Carrera
Citations in the corpus
- NURBS-based finite element analysis of functionally graded plates: Static bending, vibration, buckling and flutter (2012, methodology): “, [28] and Sohn and Kim [29, 30] investigated the nonlinear aspects of flutter characteristics using the finite element method.”
- A new four-variable refined plate theory for thermal buckling analysis of functionally graded sandwich plates (2012, background): “Sohn [24] dealt with the stabilities of FG panels subjected to combined thermal and aerodynamic loads.”
- Stress, vibration and buckling analyses of FGM plates—A state-of-the-art review (2015, methodology): “[315] to study the static and dynamic stability of FGM panels based on the FSDT and also subjected to thermal and aerodynamic loads simultaneously.”
- Thermal Buckling of Functionally Graded Plates According to a Four-Variable Refined Plate Theory (2012, methodology): “Sohn [9] dealt with the stabilities of FG panels subjected to combined thermal and aerodynamic loads.”