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Aerodynamic Characteristics at Mach Numbers From 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight
| Content Provider | University of North Texas |
|---|---|
| Author | Carmel, Melvin M. Kelly, Thomas C. Gregory, Donald T. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting an investigation of a canard-type configuration designed for supersonic cruise flight in the Unitary Plan wind tunnel. Tests were conducted over a range of angles of attack and angles of sideslip. Results regarding the effect of forebody configuration, effects of Reynolds number and transition, effect of canard and elevon deflection, and effect of vertical surfaces are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc64406 |
| Language | English |
| Publisher Date | 2019-01-04 |
| Access Restriction | Open |
| Subject Keyword | canard-type aircraft aerodynamics aircraft control |
| Content Type | Text |
| Resource Type | Report |