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Report of static test of D.H.4 (P.34) wing cellule
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | CIS US EXEC MF W87.11-2.36 | ✔ Available |
Consolidated PT-3 airplane wing cellule in high and low incidence (Airplane Branch report).
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | CIS US EXEC MF W87.11-2.626 | ✔ Available |
Effect of cellule arrangement on rate of autorotation calculated by "strip" method (Airplane Branch report).
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | CIS US EXEC MF W87.11-2.609 | ✔ Available |
Report of static test of wing cellule of Pomilio FVL-8 with unequal loads on right and left wings
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | CIS US EXEC MF W87.11-2.25 | ✔ Available |
Wind tunnel test of 1/24 scale model of Douglas O-2E-1 airplane wing cellule through 360 degrees (Airplane Branch report).
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | CIS US EXEC MF W87.11-2.612 | ✔ Available |
Discussion of stress analysis of airplane wing cellule of multi-spar type of wing construction, with special reference to loading condition of standard static test
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | CIS US EXEC MF W87.11-2.52 | ✔ Available |
