Investigation of Vibration in Rotary Wing Aircraft
Abstract
An investigation was made of vibration in rotary wing aircraft. This report presents descriptions of types of instruments for measuring vibration and systems used to record this information, methods for reducing data, and results of studies to determine the effect of vibration on components and man. Methods for attenuating some of the transmitted vibrations are suggested and de sign specification requirements on helicopter vibration are proposed.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 08, 1963
- Accession Number
- AD0412668
Entities
People
- Ronald N. Phillips
Organizations
- Naval Air Station Patuxent River