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Augmentor performance of an f100 engine model derivative engine in an f-15 airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Burcham Jr., Frank W. Walton, James T. |
| Copyright Year | 1986 |
| Description | The transient performance of the F100 engine model derivative (EMD) augmentor was evaluated in an F-15 airplane. The augmentor was a newly designed 16-segment augmentor. It was tested with a segment-1 sprayring with 90 deg fuel injection, and later with a modified segment-1 sprayring with centerline fuel injection. With the 90 deg injection, no-lights occurred at high altitudes with airspeeds of 175 knots or less; however, the results were better than when using the standard F100-PW-100 engine. With the centerline fuel injection, all transients were successful to an altitude of 15,500 meters and an airspeed of 150 knots: no failures to light, blowouts, or stalls occurred. For a first flight evaluation, the augmentor transient performance was excellent. |
| File Size | 4834599 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880014421 |
| Archival Resource Key | ark:/13960/t06x47m9s |
| Language | English |
| Publisher Date | 1986-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Thrust Augmentation Flight Tests Turbofan Engines Fuel Injection F-15 Aircraft Afterburning Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
