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Wind-tunnel investigation at low speeds of a model of the kestrel (xv-6a) vectored-trust v/stol airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Winston, M. M. Vogler, R. D. Margason, R. J. |
| Copyright Year | 1972 |
| Description | Longitudinal and lateral stability data were obtained with the model out of and in ground effect over a moving ground plane for a range of model angles of attack and sideslip at various thrust coefficients. These data were taken primarily at thrust coefficients which simulate transition speeds on the airplane between hover and 200 knots. Some data, however, represent the effect of thrust deflection at speeds up to 350 knots. Also presented are the effects of control-surface deflections and interference between the jets and free stream. |
| File Size | 38062963 |
| Page Count | 179 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720022358 |
| Archival Resource Key | ark:/13960/t9n34mj5r |
| Language | English |
| Publisher Date | 1972-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Wind Tunnel Models Aerodynamic Configurations Ground Effect Aerodynamics Aerodynamic Characteristics P-1127 Aircraft Wind Tunnel Stability 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 |
