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Effect of reynolds number and engine nacelles on the stalling characteristics of a model of a twin-engine light airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lockwood, V. E. |
| Copyright Year | 1972 |
| Description | The investigation was made on a 1/18-scale model of a twin-engine light airplane. Static longitudinal, lateral, and directional characteristics were obtained at 0 deg and plus or minus 5 deg sideslip at a Mach number of about 0.2. The angle of attack varied from about 20 deg at a Reynolds number of 0.39 times one million to 13 deg at a Reynolds number of 3.7 times one million, based on the reference chord. The effect of fixed transition, vertical and horizontal tails, and nacelle fillets was studied. |
| File Size | 15662149 |
| Page Count | 39 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730022219 |
| Archival Resource Key | ark:/13960/t6wx25559 |
| Language | English |
| Publisher Date | 1972-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Directional Stability Aerodynamic Configurations Wind Tunnel Tests Lateral Stability Aerodynamic Characteristics Light Aircraft Longitudinal Stability Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
