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V/stol tilt rotor aircraft study: wind tunnel tests of a full scale hingeless prop/rotor designed for the boeing model 222 tilt rotor aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Alexander, H. R. Magee, J. P. |
| Copyright Year | 1973 |
| Description | The rotor system designed for the Boeing Model 222 tilt rotor aircraft is a soft-in-plane hingeless rotor design, 26 feet in diameter. This rotor has completed two test programs in the NASA Ames 40' X 80' wind tunnel. The first test was a windmilling rotor test on two dynamic wing test stands. The rotor was tested up to an advance ratio equivalence of 400 knots. The second test used the NASA powered propeller test rig and data were obtained in hover, transition and low speed cruise flight. Test data were obtained in the areas of wing-rotor dynamics, rotor loads, stability and control, feedback controls, and performance to meet the test objectives. These data are presented. |
| File Size | 22131127 |
| Page Count | 889 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740007598 |
| Archival Resource Key | ark:/13960/t1jh8b195 |
| Language | English |
| Publisher Date | 1973-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Dynamic Response V/stol Aircraft Rigid Rotors Wind Tunnel Tests Rotor Aerodynamics Feedback Control Tilt Rotor Research Aircraft Program Stability Derivatives Load Tests Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
