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Volumn 4, Issue , 2004, Pages 2464-2472

Detection of fastener failure in a thermal protection system panel

Author keywords

[No Author keywords available]

Indexed keywords

COHERENCE FUNCTIONS; SENSING SIGNALS; SPACE OPERATIONS VEHICLE (SOV); STRUCTURAL HEALTH MONITORING (SHM);

EID: 11244266034     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.2004.1368041     Document Type: Conference Paper
Times cited : (9)

References (9)
  • 1
    • 0035361499 scopus 로고    scopus 로고
    • Damage diagnosis using time series analysis of vibration signals
    • H Sohn and C Farrar, "Damage diagnosis using time series analysis of vibration signals," Smart Materials and Structures, 10, 1-6, 2001.
    • (2001) Smart Materials and Structures , vol.10 , pp. 1-6
    • Sohn, H.1    Farrar, C.2
  • 4
    • 0037248049 scopus 로고    scopus 로고
    • Experimental validation of a structural health monitoring methodology: Part I. Novelty detection on a laboratory structure
    • K Worden, G Manson and D Allman, "Experimental Validation of a Structural Health Monitoring Methodology: Part I. Novelty Detection on a Laboratory Structure," J. Sound and Vibration, 259, 323-343, 2003.
    • (2003) J. Sound and Vibration , vol.259 , pp. 323-343
    • Worden, K.1    Manson, G.2    Allman, D.3
  • 5
    • 0037250871 scopus 로고    scopus 로고
    • Experimental validation of a structural health monitoring methodology: Part II. Novelty detection on a gnat aircraft
    • G Manson, K Worden, and D Allman, "Experimental Validation of a Structural Health Monitoring Methodology: Part II. Novelty Detection on a Gnat Aircraft," J. Sound and Vibration, 259, 345-363, 2003.
    • (2003) J. Sound and Vibration , vol.259 , pp. 345-363
    • Manson, G.1    Worden, K.2    Allman, D.3
  • 6
    • 0037247230 scopus 로고    scopus 로고
    • Experimental validation of a structural health monitoring methodology: Part III. Damage location on an aircraft wing
    • G Manson, K Worden, and D Allman, "Experimental Validation of a Structural Health Monitoring Methodology: Part III. Damage Location on an Aircraft Wing," J. Sound and Vibration, 259, 365-385, 2003.
    • (2003) J. Sound and Vibration , vol.259 , pp. 365-385
    • Manson, G.1    Worden, K.2    Allman, D.3
  • 7
    • 11244282570 scopus 로고    scopus 로고
    • Air Force Research Laboratory, Military Spaceplane System Technology Program Office, Version 4.2, 12 Feb
    • "System Requirements Document for a Military Spaceplane System," Air Force Research Laboratory, Military Spaceplane System Technology Program Office, Version 4.2, 12 Feb 2001.
    • (2001) System Requirements Document for A Military Spaceplane System
  • 8
    • 10044239469 scopus 로고    scopus 로고
    • Matlab version 6.5.0.180913a (R13), June 18, The Mathworks, Inc.
    • Matlab version 6.5.0.180913a (R13), June 18, 2002, Signal Processing Toolbox, Revision 1.6, The Mathworks, Inc.
    • (2002) Signal Processing Toolbox, Revision 1.6


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.