Aeroelastic Analysis of Laminated FG-CNTRC Cylindrical Panels Under Yawed Supersonic Flow.

Subjects

Subjects :

SUPERSONIC flow
FLUTTER (Aerodynamics)
FUNCTIONALLY gradient materials
POISSON'S ratio
MACH number
DIFFERENTIAL quadrature method
MATERIALS science

Details

Language :

English

ISSN :

17588251

Volume :

11

Issue :

6

Database :

Complementary Index

Journal :

International Journal of Applied Mechanics

Publication Type :

Academic Journal

Accession number :

138500988

Full Text :

https://doi.org/10.1142/S1758825119500522