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It has been suggested that one cause of a wing vibration phenomenon known as limit-cycle oscillations is the motion of shock waves in transonic flow. This article investigates whether this shock motion can be modeled effectively using a simpler aerodynamic model.
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This page is a summary of: Investigation of Shock Motion in Transonic Flow Using an Oscillating, Straked, Delta Wing, AIAA Journal, December 2018, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057456.
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