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Effect of simulated in-flight thrust reversing on vertical-tail loads of f-18 and f-15 airplane models. [conducted in the langley 16-foot transonic tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Berrier, B. L. Bare, E. A. Capone, F. J. |
| Copyright Year | 1981 |
| Description | Investigations were conducted in the Langley 16-Foot Transonic Tunnel to provide data on a 0.10-scale model of the prototype F-18 airplane and a 0.047-scale model of the F-15 three-surface configuration (canard, wing, and horizontal tails). Test data were obtained at static conditions and at Mach numbers from 0.6 to 1.2 over an angle-of-attack range from 2 deg to 15 deg. Nozzle pressure ratio was varied from jet off to about 8.0. |
| File Size | 3740663 |
| Page Count | 53 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810021548 |
| Archival Resource Key | ark:/13960/t3fz23j8b |
| Language | English |
| Publisher Date | 1981-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aircraft Models Aerodynamic Configurations Scale Models Nozzle Thrust Coefficients Thrust Reversal Structural Design Criteria F-18 Aircraft F-15 Aircraft Thrust Loads Aerodynamic Loads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
