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Effects of the spanwise, chordwise and vertical location of an external store on the aerodynamic characteristics of a 60 degree delta wing at Mach numbers of 1.41, 1.62, and 1.96
| Content Provider | University of North Texas |
|---|---|
| Author | Jacobsen, Carl R. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting an investigation in the supersonic blowdown tunnel to determine the effects of external store location on the lift, drag, and pitching-moment characteristics of a 60 degree delta wing at Mach numbers of 1.41, 1.62, and 1.96. Brief comparative tests were also made to determine the effect of changing the sweep of the strut attaching the store to the wing and of changing the chordwise location of the swept strut. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc59380 |
| Language | English |
| Publisher Date | 2018-04-02 |
| Access Restriction | Open |
| Subject Keyword | aircraft wings aircraft stores |
| Content Type | Text |
| Resource Type | Report |