CH-46 Composite Rotor Blade Flight Stress Survey Data. Volume III. Plotted Forward Rotor Blade Chord, Torsion and Absolute Loads,
Abstract
This volume contains measured steady and alternating forward rotor blade chord, torsion and absolute loads plotted versus true airspeed. The same data is tabulated in Volume 9.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1978
- Accession Number
- ADA075612
Entities
People
- J. Bendo
- R. Aiello
Organizations
- Boeing Rotorcraft Systems