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Supersonic stovl ejector aircraft from a propulsion point of view
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Glassman, A. Luidens, R. W. Plencner, R. Haller, W. |
| Copyright Year | 1984 |
| Description | A baseline supersonic STOVL ejector aircraft, its propulsion and typical operating modes is described, and important propulsion parameters are identified. Then a number of propulsion system changes are evaluated for improvement of the lift-off performance aft deflection of the ejector jet and heating of the ejector primary air either by burning or using the hot engine core flow. The possibility for cooling the footprint is illustrated for mixing or interchanging the fan and core flows, and in use of a core flow ejector. The application of a new engine concept the turbine bypass engine plus a turbocompressor to supply the ejector primary air, and thrust during takeoff combat are presented. |
| File Size | 1468264 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840016513 |
| Archival Resource Key | ark:/13960/t22c3vf8x |
| Language | English |
| Publisher Date | 1984-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Supersonic Aircraft Propulsion System Performance Ejectors Propulsive Efficiency Short Takeoff Aircraft Propulsion System Configurations Turbine Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
