CH-46 Composite Rotor Blade Flight Stress Survey Data. Volume IV. Plotted Aft Rotor Blade Angles, and Flap Loads,
Abstract
This volume contains measured steady and alternating aft rotor blade angles and flap loads plotted versus true airspeed. The same data is tabulated in Volume 10.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1978
- Accession Number
- ADA075613
Entities
People
- J. Bendo
- R. Aiello
Organizations
- Boeing Rotorcraft Systems