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SAE AIR 5450:2014-06-09
Advanced Ducted Propulsor In-Flight Thrust DeterminationMore info
The emerging ultra high bypass ratio ADP engines, with nozzle pressure ratios significantly lower, and bypass ratios significantly higher, than those of the current turbofan engines, may present new in-flight thrust determination challenges that are not specifically covered in AIR1703. This document addresses candidate methods and the additional challenges to the thrust determination for these ADP engines.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2014-06-09 |
| ICS | 49.050 : Aerospace engines and propulsion systems |
| Number of pages | 392 |
| Set | AEROPAKS10U-10 |
| Year | 2014 |
| Document history | |
| Country | USA |
| Keyword | SAE 5450;SAE AIR5450;SAE AIR5450;SAE AIR 5450 |