Aerodynamic Tests of an NACA 66(215)-116, a=0.6 Airfoil With a 0.25c Slotted Flap for the Fleetwings XA-39 Airplane (Listing Multiple Pages).
| Filename | Size | Format | Download |
|---|---|---|---|
| 19930092801.pdf | 1.2 MB | application/pdf | Download |
| Filename | Size | Format | Download |
|---|---|---|---|
| 19930092801.pdf | 1.2 MB | application/pdf | Download |