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An Investigation of Supersonic Store Interference in the Vicinity of a 22 Degree Swept Wing Fuselage Configuration at Mach Numbers of 1.61 and 2.01
| Content Provider | University of North Texas |
|---|---|
| Author | Geier, Douglas J. |
| Organization | Langley Aeronautical Laboratory |
| Description | Pressure tunnel investigation of supersonic store interference in vicinity of 22 degree swept wing fuselage configuration at Mach numbers 1.61 and 2.01. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc53117 |
| Language | English |
| Publisher Date | 2018-12-20 |
| Access Restriction | Open |
| Subject Keyword | wing-fuselage configurations aircraft stores |
| Content Type | Text |
| Resource Type | Report |