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Simulated Flight Investigation of Scaled-Speed Elastic Sweptwing Bomber and Fighter Models Coupled Wing Tip to Wing Tip
| Content Provider | University of North Texas |
|---|---|
| Author | Thompson, Robert F. |
| Organization | Langley Aeronautical Laboratory |
| Description | Memorandum presenting a wind-tunnel investigation in which dynamic models that included elastic simulation were used to study the flight characteristics of a swept-wing bomber with parasite swept-wing fighters coupled at the wing tips. The configuration is meant to represent an efficient towing arrangement whereby the operational range of fighters can be increased. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc52848 |
| Language | English |
| Publisher Date | 2019-01-03 |
| Access Restriction | Open |
| Subject Keyword | wing coupling aircraft towing |
| Content Type | Text |
| Resource Type | Report |