An approach to the design of aircraft structures with damage tolerance requirements

41st Structures, Structural Dynamics, and Materials Conference and Exhibit

Volumn , Issue , 2000, Pages

  Arrieta, Albert J ^a   Striz, Alfred G ^a   Venkayya, Vipperla B ^b  

^a UNIVERSITY OF OKLAHOMA   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT MANUFACTURE; AIRFRAMES; CRACKS; DESIGN AIDS; FATIGUE CRACK PROPAGATION; FATIGUE DAMAGE; FITS AND TOLERANCES; FORECASTING; GLOBAL OPTIMIZATION; SHAPE OPTIMIZATION; STRESS INTENSITY FACTORS; STRUCTURAL ANALYSIS; STRUCTURAL DYNAMICS; WINGS;

DAMAGE TOLERANCE ANALYSIS; FATIGUE CRACK GROWTH ANALYSIS; FATIGUE LIFE PREDICTION; GLOBAL/LOCAL FINITE ELEMENT APPROACHES; MULTIDISCIPLINARY DESIGN OPTIMIZATION; OPTIMIZATION ENVIRONMENTS; PRELIMINARY ANALYSIS; TOLERANCE REQUIREMENT;

DAMAGE TOLERANCE;

EID: 85088346460     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-1786     Document Type: Conference Paper

References (10)

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