Altitude-wind-tunnel investigation of thrust augmentation of a turbojet engine 3: performance with tail-pipe burning in standard-size tail pipe (Listing Multiple Pages).
| Filename | Size | Format | Download |
|---|---|---|---|
| 19930085647.pdf | 1.8 MB | application/pdf | Download |
| Filename | Size | Format | Download |
|---|---|---|---|
| 19930085647.pdf | 1.8 MB | application/pdf | Download |