title: Airframe structural damage detection: a non-linear structural surface intensity based technique.
abstract: The non-linear structural surface intensity (NSSI) based damage detection technique is extended to airframe applications. The selected test structure is an upper cabin airframe section from a UH-60 Blackhawk helicopter (Sikorsky Aircraft, Stratford, CT). Structural damage is simulated through an impact resonator device, designed to simulate the induced vibration effects typical of non-linear behaving damage. An experimental study is conducted to prove the applicability of NSSI on complex mechanical systems as well as to evaluate the minimum sensor and actuator requirements. The NSSI technique is shown to have high damage detection sensitivity, covering an extended substructure with a single sensing location.
authors.affiliation: Department of Aerospace Engineering, The Pennsylvania State University, University Park, Philadelphia, Pennsylvania 16802, USA. fus119@psu.edu
authors.forename: Fabio
authors.initials: F
authors.lastname: Semperlotti
authors.forename: Stephen C
authors.initials: SC
authors.lastname: Conlon
authors.forename: Andrew R
authors.initials: AR
authors.lastname: Barnard
mesh_terms: D000162:Acoustics; D000401:Aircraft; D006801:Humans; D008962:Models, Theoretical; D017711:Nonlinear Dynamics; D012449:Safety; D014732:Vibration