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Investigation of some factors affecting comparisons of wind-tunnel and flight measurements of maximum lift coefficients for a fighter-type airplane
| Content Provider | University of North Texas |
|---|---|
| Author | Davis, Don D. Jr. Sweberg, Harold H. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting a full-scale-tunnel investigation to study the effects of time rate of change of angle of attack, idling propeller operation, and Reynolds number on the maximum lift coefficient of a single-engine fighter-type airplane. Flight test measurements of maximum lift coefficient were also made and compared to wind-tunnel data. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc54745 |
| Language | English |
| Publisher Date | 2019-03-13 |
| Access Restriction | Open |
| Subject Keyword | aircraft power aerodynamics wind tunnel testing |
| Content Type | Text |
| Resource Type | Report |