8.7.2. Tension Flexure of Beams

Reference: Abbott, Richard. Analysis and Design of Composite and Metallic Flight Vehicle Structures 3 Edition, 2019

These beam solutions are taken from (NASA TM X-73305, 1975) Table B4.6.1

Where:

1. AA-SM-026-101 Beam Analysis – Tension Flexure – Cantilever Point Load at End
2. AA-SM-026-102 Beam Analysis – Tension Flexure – Cantilever UDL

3. AA-SM-026-103 Beam Analysis – Framework – Vertical Moment Fixed Support
4. AA-SM-026-104 Beam Analysis – Tension Flexure – Simply Supported Both Ends UDL
5. AA-SM-026-105 Beam Analysis – Tension Flexure – Fixed Both Ends Mid Span Load

6. AA-SM-026-106 Beam Analysis – Tension Flexure – Fixed Both Ends UDL