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Volumn 37, Issue 3, 2001, Pages 849-862

Damage-mitigating control of aircraft for enhanced structural durability

Author keywords

[No Author keywords available]

Indexed keywords

DAMAGE-MITIGATING CONTROL (DMC);

EID: 0035401428     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.953241     Document Type: Article
Times cited : (17)

References (33)
  • 2
    • 85007685430 scopus 로고
    • A Doublet-Lattice method for calculating lift distributions on oscillating surfaces in subsonic flows
    • (1969), also Errata, 7, 11 (1969), 2192
    • (1969) AIAA Journal , vol.7 , Issue.2 , pp. 279-285
    • Albano, E.1    Rodden, W.P.2
  • 21
    • 0019627111 scopus 로고
    • A crack-closure model for predicting fatigue crack growth under aircraft loading
    • Methods and Models for Predicting Fatigue Crack Growth under Random Loading, 1981
    • (1981) ASTM STP , vol.748 , pp. 53-84
    • Newman Jr., J.C.1
  • 28
    • 85168408566 scopus 로고
    • Observations on the prediction of fatigue crack growth propagation under variable-amplitude loading
    • Fatigue Crack Growth Under Spectrum Loads, 1976
    • (1976) ASTM STP , vol.595 , pp. 3-23
    • Schijve, J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.