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Fuselage and nozzle pressure distributions on a 1/12-scale f-15 propulsion model at transonic speeds. [conducted in langley 16 foot transonic tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pendergraft Jr., O. C. |
| Copyright Year | 1979 |
| Description | Static pressure coefficient distributions on the forebody, afterbody, and nozzles of a 1/12 scale F-15 propulsion model were determined. The effects of nozzle power setting and horizontal tail deflection angle on the pressure coefficient distributions were investigated. |
| File Size | 6828736 |
| Page Count | 141 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800002790 |
| Archival Resource Key | ark:/13960/t8cg4hr19 |
| Language | English |
| Publisher Date | 1979-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aircraft Models Propulsion System Performance Exhaust Nozzles Nozzle Flow Transonic Wind Tunnels Flow Distribution Wind Tunnel Tests Pressure Distribution Fuselages F-15 Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
