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Flight Investigation of the Effect of Underwing Propulsive Jets on the Lift, Drag, and Longitudinal Stability of a Delta-Wing Configuration at Mach Numbers From 1.23 to 1.62
| Content Provider | University of North Texas |
|---|---|
| Author | Falanga, Ralph A. Judd, Joseph H. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report discussing testing of a multijet 60 degree delta-wing airplane configuration with twin-engine exhausts at specified locations under the wing. Data was obtained for jet-on and jet-off conditions between a range of Mach numbers. Results are presented for the effect of jet on drag, jet effect on lift, static longitudinal stability, and dynamic longitudinal stability. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc61605 |
| Language | English |
| Publisher Date | 2019-01-10 |
| Access Restriction | Open |
| Subject Keyword | aerodynamics drag coefficients delta-wing airplanes |
| Content Type | Text |
| Resource Type | Report |