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Comparison of Locked-Rotor and Windmilling Drag Characteristics of an Axial-Flow-Compressor Type Turbojet Engine
| Content Provider | University of North Texas |
|---|---|
| Author | Vincent, K. R. Huntley, S. C. Wilsted, H. D. |
| Organization | Lewis Flight Propulsion Laboratory |
| Description | The internal drag of an axial-flow turbojet engine with the rotor locked in place to prevent windmilling and with the engine windmilling was obtained over a range of simulated Mach numbers. The corrected internal drag of the engine with the locked rotor was 210 pounds or only 46 percent of the windmilling drag at a flight Mach number of 0.8. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc59320 |
| Language | English |
| Publisher Date | 2019-01-07 |
| Access Restriction | Open |
| Subject Keyword | turbojet engines internal drag |
| Content Type | Text |
| Resource Type | Report |
