Response of a Store with Tunable Natural Frequencies in Compressible Cavity Flow
Fluid-structure interactions that occur during aircraft internal store carriage were experimentally explored at Mach 0.94 and 1.47 using a generic, aerodynamic store installed in a rectangular cavity having a length-to-depth ratio of 7. Similar to previous studies using a cylindrical store, the aero...
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| creator | Wagner, Justin L. Casper, Katya Marie Beresh, Steven J. Hunter, Patrick S. Spillers, Russell Wayne Henfling, John F. |
| description | Fluid-structure interactions that occur during aircraft internal store carriage were experimentally explored at Mach 0.94 and 1.47 using a generic, aerodynamic store installed in a rectangular cavity having a length-to-depth ratio of 7. Similar to previous studies using a cylindrical store, the aerodynamic store responded to the cavity flow at its natural structural frequencies, and it exhibited a directionally dependent response to cavity resonance. Moreover, cavity tones excited the store in the streamwise and wall-normal directions consistently, whereas the spanwise response was much more limited. |
| doi_str_mv | 10.2514/6.2015-1293 |
| format | Conference Proceeding |
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| fulltext | fulltext |
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| ispartof | 53rd AIAA Aerospace Sciences Meeting, 2015, Vol.2105 |
| issn | 0001-1452 1533-385X |
| language | eng |
| recordid | cdi_osti_scitechconnect_1237696 |
| source | Alma/SFX Local Collection |
| subjects | ENGINEERING |
| title | Response of a Store with Tunable Natural Frequencies in Compressible Cavity Flow |
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