Optimum design of composite plate wings for aeroelastic characteristics using lamination parameters

By M. Kameyama, Hisao Fukunaga. 2007

158 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Civil and Structural Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/40bb40604fe8a7af5a66bc1f3856e044c8ab2276

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Damiano Pasini
2. L. Lessard
3. Hossein Ghiasi
4. Paul M. Weaver
5. S. Vidoli
6. Kazem Fayazbakhsh

In Civil and Structural Engineering

1. L. Lessard
2. Damiano Pasini
3. Paul M. Weaver
4. Paul Kealy
5. J. Cooper
6. Hossein Ghiasi
7. O. Stodieck
8. S. Vidoli

In Mechanics of Materials

1. Damiano Pasini
2. L. Lessard
3. Paul M. Weaver
4. Paul Kealy
5. J. Cooper
6. Hossein Ghiasi
7. O. Stodieck
8. S. Vidoli

Citations in the corpus

• Stiffness Optimization of Composite Wings with Aeroelastic Constraints (2012, unknown): “Kameyama and Fukunaga [17] demonstrated the mass optimization of a platelike wing with aeroelastic constraints.”
• Improved aeroelastic tailoring using tow-steered composites (2013, background): “Some examples of composite wing aeroelastic tailoring include the increase of the divergence airspeed for forward-swept wing designs [2], weight reduction [3], drag reduction [4], gust response [5,6], optimum flutter characteristics [7], and maintaining static strength, buckling constraints, and opt”
• Optimum stacking sequence design of composite materials Part I: Constant stiffness design (2009, background): “Autio [110], Kameyama and Fukunaga [111], Enrique et al.”