Indirect approaches to individual aircraft structural monitoring

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 218, Issue 5, 2004, Pages 329-346

  Wallace, M ^a   Azzam, H ^a,c   Newman, S ^b  

^a Smiths Aerospace Electronic Systems   (United Kingdom)

^b UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

^c Smiths Aerosp Electron Syst S ^*  (United Kingdom)

Author keywords

Aircraft structural monitoring; Individual aircraft tracking (IAT); Recorded flight parameters

Indexed keywords

DATA ACQUISITION; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; PRINCIPAL COMPONENT ANALYSIS; STRAIN GAGES; STRUCTURAL LOADS;

AIRCRAFT STRUCTURAL MONITORING; DESIGN AUTHORITY (DA); INDIVIDUAL AIRCRAFT TRACKING (IAT); RECORDED FLIGHT PARAMETERS;

AIRCRAFT;

EID: 10644262262     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/0954410042467059     Document Type: Article

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