Sungsoo Na

Tech University of Korea

Papers

1

Total Citations

7

H-Index

1

About

Sungsoo Na is a distinguished researcher in aerospace structural dynamics, with a primary focus on the vibrational behavior and aeroelastic stability of advanced composite aircraft wings. His work is foundational in modeling thin-walled beam structures, particularly those made from anisotropic composite materials. Na’s key contribution lies in incorporating non-classical effects—such as transverse shear deformation and warping inhibition—into the dynamic analysis of doubly-tapered wings, providing a more accurate framework for predicting structural responses under aerodynamic loads. His seminal 1999 paper, "Dynamic Behavior of Aircraft Wings Modeled as Doubly-Tapered Composite Thin-Walled Beams," has garnered 7 citations, serving as a critical reference for engineers and researchers seeking to optimize lightweight, high-performance wing designs. By bridging theoretical mechanics with practical aerospace applications, Na has advanced the understanding of how material anisotropy and geometric tapering influence flutter, vibration, and overall structural integrity. His work continues to inform the development of safer, more efficient aircraft, making him a respected figure in the field of composite structural dynamics.

Research Focus

Key Achievements

1
H-Index
1
Papers
7
Total Citations
7
Avg Citations/Paper
🏆 Most Cited Paper
Dynamic Behavior of Aircraft Wings Modeled as Doubly-Tapered Composite Thin-Walled Beams
7 citations · 1999
📈 Most Prolific Year: 1999 (1 Papers)
🤝 Key Collaborators: 1
🏛 Institutions: Tech University of Korea

Top Papers

  1. 1

Key Collaborators

Contact & Links

Available for collaboration
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