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46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Royal Australian Air Force (RAAF) F/A-18 flight flutter test data is presented and analyzed using various techniques. The data includes high-quality measurements of forced responses and limit cycle oscillation (LCO) phenomena. Standard correlation and power spectral density (PSD) techniques are applied to the data and presented. Novel applications of experimentally-identified impulse responses and higher-order spectral techniques are also applied to the data and presented. The goal of thisdoi:10.2514/6.2005-2014 fatcat:lhj25lvwkbg6lbkssqrt5rbmiu