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Study of aerodynamic technology for single-cruise engine v/stol fighter/attack aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Roush, R. T. Powers, S. A. Driggers, H. H. |
| Copyright Year | 1982 |
| Description | A conceptual design analysis is performed on a single engine V/STOL supersonic fighter/attack concept powered by a series flow tandem fan propulsion system. Forward and aft mounted fans have independent flow paths for V/STOL operation and series flow in high speed flight. Mission, combat and V/STOL performance is calculated. Detailed aerodynamic estimates are made and aerodynamic uncertainties associated with the configuration and estimation methods identified. A wind tunnel research program is developed to resolve principal uncertainties and establish a data base for the baseline configuration and parametric variations. |
| File Size | 8066220 |
| Page Count | 213 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840020668 |
| Archival Resource Key | ark:/13960/t79s6kq3m |
| Language | English |
| Publisher Date | 1982-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Nozzle Geometry V/stol Aircraft Engine Design Wind Tunnel Tests Turbofan Engines Design Analysis Aerodynamic Characteristics Propulsion System Configurations Prediction Analysis Techniques Data Bases Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
