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Effects of inlet distortion on a static pressure probe mounted on the engine hub in an f-15 airplane (Document No: 19850014083)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mackall, K. G. Hughes, D. L. Myers, L. P. |
| Copyright Year | 1985 |
| Description | An inlet static pressure (PS2) probe was mounted on the hub of an F100 engine in an F-15 airplane. Flight test results showed that for low distortion conditions, the ratio of engine-face total pressure to static pressure agreed well with previous altitude facility data. Off-schedule operation of the inlet third ramp angle caused increased distortion of the inlet airflow during steady-state flight conditions. Data are shown for inlet third ramp excursions leading to engine stall. The relationships of inlet face total to static pressure ratio as a function of several distortion descriptors are also described. |
| File Size | 4591095 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850014083 |
| Archival Resource Key | ark:/13960/t21c6vq4d |
| Language | English |
| Publisher Date | 1985-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Static Pressure Flight Tests Engine Failure Turbofan Engines Inlet Flow Fuel Flow Pressure Measurement Aircraft Engines Angle of Attack F-15 Aircraft Mach Number 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 |
