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Flight investigation of the effects of horizontal-tail height, moment of inertia, and control effectiveness on the pitch-up characteristics of a 35 degree swept-wing fighter airplane at high subsonic speeds
| Content Provider | University of North Texas |
|---|---|
| Author | McFadden, Norman M. Heinle, Donovan R. |
| Organization | Ames Aeronautical Laboratory (U.S.) |
| Description | Report presenting a flight investigation conducted on a 35 degree swept-wing fighter airplane with two different horizontal-tail heights. The longitudinal stability and buffet characteristics were compared for the two configurations. Results regarding longitudinal stability, buffet, and pitch-up intensity are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc60573 |
| Language | English |
| Publisher Date | 2018-06-18 |
| Access Restriction | Open |
| Subject Keyword | horizontal tails aircraft stability |
| Content Type | Text |
| Resource Type | Report |