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Vce test bed engine for supersonic cruise research
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Vdoviak, J. W. Ebacher, J. A. |
| Copyright Year | 1980 |
| Description | Various design concepts for a variable cycle engine applicable to a supersonic, mixed mission propulsion system which would combine the merits of a turbofan at subsonic operating conditions with those of a turbojet for supersonic operating conditions are briefly examined. In particular the integration of the variable area bypass injector with the core driven (aft fan block) fan stage is discussed and the technical benefits of the configuration are summarized. |
| File Size | 2051952 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810009472 |
| Archival Resource Key | ark:/13960/t3hx6522s |
| Language | English |
| Publisher Date | 1980-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Variable Cycle Engines Engine Design Noise Reduction Supersonic Cruise Aircraft Research Engine Inlets Fuel Consumption Engine Tests Engine Parts Aerodynamic Characteristics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
