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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 | Report presenting an investigation in the supersonic pressure tunnel at Mach numbers 1.61 and 2.01 in which separate forces and moments were measured on a store (with five components), on a 22 degree swept wing (three components), and on a 22 degree swept-wing-fuselage combination (three components) for a range of store positions. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc63937 |
| Language | English |
| Publisher Date | 2018-05-02 |
| Access Restriction | Open |
| Subject Keyword | pressure distributions aircraft stores |
| Content Type | Text |
| Resource Type | Report |