High Speed Wind-Tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 1/16-Scale Model of the D-558-2 Research Airplane at High Subsonic Mach Number and at a Mach Number of 1.2 (Listing Multiple Pages).
| Filename | Size | Format | Download |
|---|---|---|---|
| 19930085883.pdf | 2.2 MB | application/pdf | Download |