| Download | - View final version: Estimated performance of derwent V with oversize exhaust nozzles (PDF, 2.6 MiB)
|
|---|
| DOI | Resolve DOI: https://doi.org/10.4224/40003784 |
|---|
| Author | Search for: Smith, E. L.1 |
|---|
| Affiliation | - National Research Council Canada. National Aeronautical Establishment
|
|---|
| Format | Text, Memorandum |
|---|
| Physical description | 6 p. |
|---|
| Abstract | The following memorandum has been prepared to enable performance estimates to be made for a Meteor aircraft when equipped with Derwent V (or VIII) engines, fitted with reheat systems having a cold loss of about 3 percent and with various oversize exhaust nozzles. |
|---|
| Publication date | 1953-04-08 |
|---|
| Publisher | National Research Council Canada |
|---|
| Series | |
|---|
| Language | English |
|---|
| Peer reviewed | No |
|---|
| Export citation | Export as RIS |
|---|
| Report a correction | Report a correction (opens in a new tab) |
|---|
| Record identifier | c9fb07f0-c343-4f63-9ace-2e0edbae5a52 |
|---|
| Record created | 2025-10-14 |
|---|
| Record modified | 2025-11-03 |
|---|
