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Wind-tunnel tests of the xv-15 tilt rotor aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Maisel, M. D. Weiberg, J. A. |
| Copyright Year | 1980 |
| Description | The XV-15 aircraft was tested in the Ames 40 by 80 Foot Wind Tunnel for preliminary evaluation of aerodynamic and aeroelastic characteristics prior to flight. The tests were undertaken to investigate the aircraft performance, stability, control and structural loads for flight modes from helicopter through transition and airplane mode up to the tunnel capability of 170 knots. Results from these tests are presented. |
| File Size | 7026026 |
| Page Count | 138 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800015802 |
| Archival Resource Key | ark:/13960/t7wm63c89 |
| Language | English |
| Publisher Date | 1980-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Dynamic Structural Analysis Tables Data Aerodynamic Configurations Xv-15 Aircraft Wind Tunnel Tests Aircraft Performance Tilt Rotor Research Aircraft Program Aeroelasticity Aerodynamic Characteristics Data Reduction Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |