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V/stol tilt rotor aircraft study. volume 10: performance and stability test of a 1-14.622 froude scaled boeing vertol model 222 tilt rotor aircraft (phase 1)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mutter, H. Alexander, H. R. McHugh, F. J. Eason, W. |
| Copyright Year | 1973 |
| Description | Wind tunnel test data obtained from a 1/4.622 Froude scale Boeing Model 222 with a full span, two prop, tilt rotor, powered model in the Boeing V/STOL wind tunnel are reported. Data were taken in transition and cruise flight conditions and include performance, stability and control and blade loads information. The effects of the rotors, tail surfaces and airframe on the performance and stability are isolated as are the effects of the airframe on the rotors. |
| File Size | 71091490 |
| Page Count | 521 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740005614 |
| Archival Resource Key | ark:/13960/t0sr3nd0w |
| Language | English |
| Publisher Date | 1973-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Aircraft Stability V/stol Aircraft Aerodynamic Configurations Rotors Control Surfaces Wind Tunnel Tests Aircraft Performance Wind Tunnel Models Aerodynamic Characteristics Tilting Rotors Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
