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A study on the crashworthiness design and analysis for military helicopter

✍ Scribed by Jang-Wook Hur, Jae-Ho Jang

Book ID
120908209
Publisher
Korean Society for Precision Engineering
Year
2013
Tongue
English
Weight
814 KB
Volume
14
Category
Article
ISSN
1229-8557

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πŸ“œ SIMILAR VOLUMES

[American Institute of Aeronautics and A
[American Institute of Aeronautics and Astronautics 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization - Atlanta, Georgia ()] 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization - Size and Topological Optimization for Crashworthiness Design of Helicopter Subfloor
✍ Bisagni, Chiara; Lanzi, Luca; Ricci, Sergio πŸ“‚ Article πŸ“… 2002 πŸ› American Institute of Aeronautics and Astronautics βš– 327 KB
OPTIMUM DESIGN OF A HELICOPTER ROTOR FOR
OPTIMUM DESIGN OF A HELICOPTER ROTOR FOR LOW VIBRATION USING AEROELASTIC ANALYSIS AND RESPONSE SURFACE METHODS
✍ R. GANGULI πŸ“‚ Article πŸ“… 2002 πŸ› Elsevier Science 🌐 English βš– 604 KB

An aeroelastic analysis based on finite elements in space and time is used to model the helicopter rotor in forward flight. The rotor blade is represented as an elastic cantilever beam undergoing flap and lag bending, elastic torsion and axial deformations. The objective of the improved design is to