Search Results
Showing 1 - 2 of 2 results
Search Results
Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:208191 | ✔ Available |
Evaluation of a composite sandwich fuselage side panel with damage and subjected to internal pressure
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:110309 | ✔ Available |