Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured on the Wing of the Bell X-1 Airplane in Level Flight at Mach Numbers From 0.79 to 1.00 and in a Pull-Up at a Mach Number of 0.96 (Listing Multiple Pages).
| Filename | Size | Format | Download |
|---|---|---|---|
| 19930086333.pdf | 1.6 MB | application/pdf | Download |