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Volumn 236, Issue 1, 2000, Pages 49-60

Non-linear vibration method for detection of fatigue cracks in aircraft wings

Author keywords

[No Author keywords available]

Indexed keywords

BENDING (DEFORMATION); CRACKS; DYNAMIC RESPONSE; ELASTICITY; FATIGUE OF MATERIALS; MATHEMATICAL MODELS; NONDESTRUCTIVE EXAMINATION; WINGS;

EID: 0034272303     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.2000.2981     Document Type: Article
Times cited : (84)

References (21)
  • 3
    • 85031565836 scopus 로고
    • Utilization of dynamic properties for non-destructive testing of aviation structures (in Russian)
    • Riga: Zinatne. p. 97-100
    • MILOV A. B., NEVSKY YU. N., STRAKHOV G. I., UKHOV YU. G. Utilization of dynamic properties for non-destructive testing of aviation structures (in Russian). The Problems of Dynamics and Strength. 1983;Zinatne, Riga. p. 97-100.
    • (1983) The Problems of Dynamics and Strength
    • Milov, A.B.1    Nevsky, Yu.N.2    Strakhov, G.I.3    Ukhov, Yu.G.4
  • 4
    • 0039522796 scopus 로고
    • The influence of fatigue damages in built-up construction on damping
    • SIDOROV O. T. The influence of fatigue damages in built-up construction on damping. Soviet Journal of Non-destructive Testing. 18:1982;75-78.
    • (1982) Soviet Journal of Non-destructive Testing , vol.18 , pp. 75-78
    • Sidorov, O.T.1
  • 7
    • 0000059529 scopus 로고    scopus 로고
    • Detection of fatigue cracks in flexible geometrically non-linear bars by vibration monitoring
    • TSYFANSKY S. L., BERESNEVICH V. I. Detection of fatigue cracks in flexible geometrically non-linear bars by vibration monitoring. Journal of Sound and Vibration. 213:1998;159-168.
    • (1998) Journal of Sound and Vibration , vol.213 , pp. 159-168
    • Tsyfansky, S.L.1    Beresnevich, V.I.2
  • 8
  • 16
    • 0003390962 scopus 로고
    • Dynamic behaviour of the Laval rotor with a cracked hollow shaft - A comparison of crack models
    • GASCH R., PERSON M., WEITZ B. Dynamic behaviour of the Laval rotor with a cracked hollow shaft - a comparison of crack models. Institute of Mechanical Engineering. C 31/88:1983;463-472.
    • (1983) Institute of Mechanical Engineering. C , vol.31-88 , pp. 463-472
    • Gasch, R.1    Person, M.2    Weitz, B.3
  • 17
    • 85031571321 scopus 로고
    • On the method for detection of damages in aircraft wing by the analysis of its nonlinear vibrations (in Russian)
    • Riga: Zinatne. p. 3-10
    • TSYFANSKY S. L., OZHIGANOV V. M., MILOV A. B., NEVSKY YU. N. On the method for detection of damages in aircraft wing by the analysis of its nonlinear vibrations (in Russian). The Problems of Dynamics and Strength. 1981;Zinatne, Riga. p. 3-10.
    • (1981) The Problems of Dynamics and Strength
    • Tsyfansky, S.L.1    Ozhiganov, V.M.2    Milov, A.B.3    Nevsky, Yu.N.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.