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Effects of inlet distortion on a static pressure probe mounted on the engine hub in an f-15 airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mackall, K. G. Hughes, D. L. |
| Copyright Year | 1984 |
| Description | Problems encountered in obtaining good engine face pressure data were studied. A single static measurement located upstream of the engine hub in the stream flow was found to provide a pressure signal suitable for engine control. Two identical probes for measuring fan inlet static (PS2) pressure were designed and mounted on the hub of the left F100-PW-100 turbofan engine installed in the F-15 test aircraft for flight evaluation. The probe is used as a static pressure sensor for a digital engine control system. |
| File Size | 660279 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860015876 |
| Archival Resource Key | ark:/13960/t0tr0r92x |
| Language | English |
| Publisher Date | 1984-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Pressure Sensors Static Pressure Flight Tests Flow Distortion Digital Techniques Measuring Instruments Engine Control Turbofan Engines Inlet Flow Numerical Control F-15 Aircraft Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |