CH-46 Composite Rotor Blade Flight Stress Survey Data. Volume V. Plotted Aft Rotor Blade Chord Torsion and Absolute Loads,
Abstract
This volume contains measured steady and alternating aft rotor blade chord, torsion and absolute 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
- ADA075614
Entities
People
- J. Bendo
- R. Aiello
Organizations
- Boeing Rotorcraft Systems