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Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 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 | An investigation has been made in the Langley 9- by 12-inch supersonic blowdown tunnel to determine the effects of external-store location on the lift, drag, and pitching-moment characteristics of a 45 degree sweptback wing at Mach numbers of 1.41, 1.62, and 1.96. The spanwise, chordwise, and vertical location of a Douglas-Aircraft Company, Inc., store of fineness ratio 8.58 was systematically varied over the outer 60 percent of the wing semispan. A brief investigation of strut sweep angle was also made. The test Reynolds number based on the wing mean aerodynamic chord ranged from 1.3 x 10(exp 6) to 1.5 x 10(exp 6). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc64554 |
| Language | English |
| Publisher Date | 2018-04-02 |
| Access Restriction | Open |
| Subject Keyword | aircraft stores aerodynamics aircraft wings |
| Content Type | Text |
| Resource Type | Report |
