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Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a tip-to-tip bomber-fighter coupled airplane configuration
| Content Provider | University of North Texas |
|---|---|
| Author | Bennett, Charles V. Cadman, Robert B. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting an investigation in the free-flight tunnel to determine the dynamic lateral stability and control characteristics of a coupled airplane configuration with simplified fighter models attached to the wing tips of a simplified bomber model. The configuration is meant to represent fighter airplanes carried on the wing tips of a bomber airplane to provide fighter protection for the bomber or for in-flight fueling. Results regarding the fighters attached with freedom in roll, with freedom in roll and pitch, and with freedom in roll, pitch, and yaw are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc58802 |
| Language | English |
| Publisher Date | 2018-07-05 |
| Access Restriction | Open |
| Subject Keyword | aircraft stability aircraft control coupled airplane configurations |
| Content Type | Text |
| Resource Type | Report |