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Supersonic aerodynamic characteristics of an advanced f-16 derivative aircraft configuration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Fox, Mike C. Forrest, Dana K. |
| Copyright Year | 1993 |
| Description | A supersonic wind tunnel investigation was conducted in the NASA Langley Unitary Plan Wind Tunnel on an advanced derivative configuration of the United States Air Force F-16 fighter. Longitudinal and lateral directional force and moment data were obtained at Mach numbers of 1.60 to 2.16 to evaluate basic performance parameters and control effectiveness. The aerodynamic characteristics for the F-16 derivative model were compared with the data obtained for the F-16C model and also with a previously tested generic wing model that features an identical plan form shape and similar twist distribution. |
| File Size | 8014225 |
| Page Count | 123 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930022544 |
| Archival Resource Key | ark:/13960/t1rg0nt48 |
| Language | English |
| Publisher Date | 1993-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aircraft Models Delta Wings Supersonic Wind Tunnels Wind Tunnel Tests Controllability Wind Tunnel Models F-16 Aircraft Aerodynamic Characteristics Aircraft Configurations Mach Number Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |