Stress Analysis of Control System,
Abstract
Analysis is made of the control system of the XB-36 bomber. This analysis is an addendum to the stress analysis previously given for the YB-36 and B-36A bombers. Attention has been given to the control column, aileron controls, elevator controls, elevator trim tab system, rudder controls and brake pedal system, rudder control system and rudder trim tab system. A summary of the margins of safety is included.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1947
- Accession Number
- ADB812166
Entities
People
- E. M. Asplund
- G. E. Tom
- R. G. Pollock
Organizations
- General Dynamics