Ch-46 Composite Rotor Blade Flight Stress Survey Data, Volume XII. Tabulated Forward and Aft Rotor Shaft Loads, Load Factor, Pitch and Roll Attitude and Rotor RPM,
Abstract
This volume contains measured steady and alternating forward and aft rotor shaft loads tabulated by flight and event number. Maximum and minimum forward and aft shaft torque values are included in this grouping. The steady and alternating data is plotted versus true airspeed and can be found in Volume 8. In addition, this volume contains measured (steady, maximum and minimum) load factor, pitch/roll attitude, and rotor rpm tabulated by flight and event number.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1978
- Accession Number
- ADA075621
Entities
People
- J. Bendo
- R. Aiello
Organizations
- Boeing Rotorcraft Systems