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Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Banks, Daniel W. |
| Copyright Year | 1988 |
| Description | An experimental investigation of the in-ground effect aerodynamic characteristics and predicted landing-ground-roll performance of wing-canard fighter configuration with a secondary nozzle thrust reverser was completed. These tests were conducted in the Langley 14 by 22 foot Subsonic Wind Tunnel using a model equipped with a pneumatic jet for thrust simulation of nozzle pressure ratios up to 4.0. The model was tested in the landing rollout configuration at approx. wheel touchdown height for a range of decreasing dynamic pressure from 50 psf down to 10 psf. Landing-ground-roll predictions of the configuration were calculated using the wind tunnel results. |
| File Size | 10505207 |
| Page Count | 131 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880020368 |
| Archival Resource Key | ark:/13960/t1kh5gj9q |
| Language | English |
| Publisher Date | 1988-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aircraft Landing Canard Configurations Cascade Flow Aerodynamic Configurations Jet Thrust Nozzle Flow Wind Tunnel Tests Pressure Ratio Thrust Reversal Short Takeoff Aircraft Ground Effect Aerodynamics Roll Aircraft Configurations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
