Supersonic flutter of shear deformable laminated composite flat panels
โ Scribed by V. Birman; L. Librescu
- Book ID
- 107821283
- Publisher
- Elsevier Science
- Year
- 1990
- Tongue
- English
- Weight
- 677 KB
- Volume
- 139
- Category
- Article
- ISSN
- 0022-460X
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
The dynamic instability resulting from a high-supersonic flow over a simply supported laminated flat panel subjected to uniform in-plane edge compression is studied. The structural model incorporates geometrical non-linearities, transverse shear deformation, and transverse normal stress effects, and
Flutter of hybrid laminated flat panels in supersonic flow is studied by using first order shear deformation theory in conjunction with the assumed mode method. Both the quasi-static approximation and piston theory are used for aerodynamic force calculations at supersonic speeds. The flutter stabili