To obtain access to full text of journal and articles you must register!
- Article name
- Application of polymeric composite materials in helicopter designs for vibration strength raise
- Authors
- SMOTROVA S. A., , svetlana.smotrova@tsagi.ru, Central Aerohydrodynamic Institute named after professor N. E. Zhukovsky, Moscow, Russia
SMOTROV A. V., , andrey.smotrov@tsagi.ru, Central Aerohydrodynamic Institute named after professor N. E. Zhukovsky, Moscow, Russia
KOVALEV I. E., , kovalev@tsagi.ru, Central Aerohydrodynamic Institute named after professor N. E. Zhukovsky, Moscow, Russia
- Keywords
- polymer composite materials / helicopter designs / vibration strength / ground vibration tests / finite element method
- Year
- 2017 Issue 4 Pages 28 - 36
- Code EDN
- Code DOI
- Abstract
- The comparative analysis of dynamic characteristics polymeric composite materials (PCM) aviation load-bearing designs is made. Dynamic characteristics of these designs have been experimentally registered by ground vibration tests and calculated by finite element method. For comparison the data defined for blades of the steering rotor, fabricated as from PCM, and manufactured of metal alloys is chosen.
- Text
- To obtain access to full text of journal and articles you must register!
- Buy
