Skin design studies for variable camber morphing airfoils

By Farhan Gandhi, P. Anusonti-Inthra. 2008

141 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/f77787888b975e2175460ee644be9bcf21f57743

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. K. R. Olympio
2. Farhan Gandhi

In Computational Mechanics

1. K. R. Olympio
2. Farhan Gandhi

Citations in the corpus

• Flexible Skins for Morphing Aircraft Using Cellular Honeycomb Cores (2010, background): “Results from Gandhi and Anusonti-Inthra (2007) indicate that strain capability of about 2% would be more than adequate for airfoil camber applications.”
• Zero Poisson’s Ratio Cellular Honeycombs for Flex Skins Undergoing One-Dimensional Morphing (2010, background): “Thus, for material yield strain of the order of 0.25% (common for metallic engineering materials), the maximum global strains of the honeycomb would be 2.5 3%, which would be sufficient for airfoil camber morphing applications (Gandhi and Anusonti-Inthra, 2007).”