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SAE ARP 704A:1997-05-01
Helicopter Engine-Rotor System CompatibilityMore info
This SAE Aerospace Recommended Practice (ARP) recommends a methodology to be used for the design, analysis and test evaluation of modern helicopter gas turbine propulsion system stability and transient response characteristics. This methodology utilizes the computational power of modern digital computers to more thoroughly analyze, simulate and bench-test the helicopter engine/rotor system speed control loop over the flight envelope. This up-front work results in significantly less effort expended during flight test and delivers a more effective system into service.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| ICS | 49.050 : Aerospace engines and propulsion systems |
| Number of pages | 4 |
| Replace | SAE ARP 704:1962-06-30 |
| Set | AEROPAKS10U-10 |
| Year | 1990 |
| Document history | SAE ARP 704:1962-06-30 |
| Country | USA |
| Keyword | SAE 704;SAE ARP704A;SAE ARP704A;SAE ARP 704 |