Loading...
Please wait, while we are loading the content...
Similar Documents
The effect of inlet installation on the zero-lift drag of a 60 degree delta-wing-body configuration from flight tests at Mach numbers from 0.8 to 1.86
| Content Provider | University of North Texas |
|---|---|
| Author | Merlet, Charles F. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting zero-lift drag results for two 60 degree delta-wing configurations with air inlets. One had twin conical-shock semi-circular scoops just ahead of the wing-body juncture and one had a modified wing section over the inboard portion to allow installation of modified triangular inlets in the wing leading edge. Results regarding the drag coefficients and mass-flow ratios are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc61586 |
| Language | English |
| Publisher Date | 2018-04-11 |
| Access Restriction | Open |
| Subject Keyword | aircraft inlets aerodynamics drag coefficients |
| Content Type | Text |
| Resource Type | Report |