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Longitudinal-control effectiveness and downwash characteristics at transonic speeds of a 1/30-scale semispan model of the Bell X-5 airplane as determined by the NACA wing-flow method
| Content Provider | University of North Texas |
|---|---|
| Author | Silsby, Norman S. Morris, Garland J. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting an investigation at transonic speeds using the wing-flow method to determine the longitudinal-control effectiveness and downwash characteristics of a 1/30-scale semispan model of the Bell X-5 airplane with three different degrees of sweepback. Lift, drag, and pitching moment are presented for various angles of attack for several horizontal-tail settings and with the tail off for each angle of sweep tested. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc59446 |
| Language | English |
| Publisher Date | 2018-05-09 |
| Access Restriction | Open |
| Subject Keyword | Bell X-5 sweptback wings |
| Content Type | Text |
| Resource Type | Report |