Effect of Air-Flow Distribution and Total-Pressure Loss on Performance of One-Sixth Segment of Turbojet Combuster (All Formats)
This item is available in multiple formats. Choose one below.
| Number of items: | 51 |
|---|---|
| Filetype: | tif (image) |
| Number of items: | 1 |
|---|---|
| Filetype: | pdf (file) |