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Volumn , Issue , 2004, Pages

Accelerated flutter testing: A possible technique to expedite flutter testing for new aircraft

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EID: 84896856632     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (2)

References (30)
  • 2
    • 84896880961 scopus 로고
    • Application Note 9, Rockland Scientific Corp., December
    • George F. Lang, Understanding Vibration Measurements, Application Note 9, Rockland Scientific Corp., December 1978.
    • (1978) Understanding Vibration Measurements
    • Lang, G.F.1
  • 4
    • 0342643308 scopus 로고
    • Prentice-Hall Incorporated, Englewood Cliffs, New Jersey
    • Stiltz, Harry L., Aerospace Telemetry, Prentice-Hall Incorporated, Englewood Cliffs, New Jersey, 1961.
    • (1961) Aerospace Telemetry
    • Stiltz, H.L.1
  • 5
    • 84896829755 scopus 로고
    • An Introduction 3rd ed., Instrument Society of America
    • Strock, O.J., Telemetry Computer Science, An Introduction 3rd ed., Instrument Society of America, 1983.
    • (1983) Telemetry Computer Science
    • Strock, O.J.1
  • 8
    • 84896882247 scopus 로고
    • IRE Transactions on Automatic Control Dec
    • E. C. Levy, Complex Curve Fitting, IRE Transactions on Automatic Control, Vol AC 4, No. 1, pp 327, Dec 1958
    • (1958) Complex Curve Fitting , vol.4 , Issue.1 , pp. 327
    • Levy, E.C.1
  • 13
    • 84941531309 scopus 로고
    • Application Note 243, Hewlett-Packard Company, Palo Alto, California
    • The Fundamentals of Signal Analysis, Application Note 243, Hewlett-Packard Company, Palo Alto, California, 1985.
    • (1985) The Fundamentals of Signal Analysis
  • 23
    • 85007688839 scopus 로고
    • Prediction of Flutter Onset Speed Based on Flight Testing at Subcritical Speeds
    • Norman H. Zimmerman and Jason T. Weissenburger, Prediction of Flutter Onset Speed Based on Flight Testing at Subcritical Speeds, J. Aircraft, Vol. 1, No. 4, 1963.
    • (1963) J. Aircraft , vol.1 , Issue.4
    • Zimmerman, N.H.1    Weissenburger, J.T.2
  • 24
    • 0022131039 scopus 로고
    • An Eigensystem Realization Algorithm (ERA) for Modal Parameter Identification and Model Reduction
    • J. N. Juang and R. S. Pappa, An Eigensystem Realization Algorithm (ERA) for Modal Parameter Identification and Model Reduction, J. of Guidance, Control, and Dynamics 1985, 8:620-627.
    • (1985) J. of Guidance Control, and Dynamics , vol.8 , pp. 620-627
    • Juang, J.N.1    Pappa, R.S.2
  • 25
    • 85003365433 scopus 로고
    • Efficient Computation of the Eigensystem Realization Algotithm
    • L. D. Peterson, Efficient Computation of the Eigensystem Realization Algotithm, J. Guidance, Control, and Dynamics 1995, 18:395-403.
    • (1995) J. Guidance, Control, and Dynamics , vol.18 , pp. 395-403
    • Peterson, L.D.1
  • 26
    • 0005093697 scopus 로고    scopus 로고
    • The Statistical Sensitivity of Experimental Modal Frequencies and Damping Ratios to Measurement Noise
    • AIAA, Aerospace Sciences Meeting and Exhibit, 37, th, Reno, NV, Jan 11-14, 1999
    • L. D. Peterson, S. J. Bullock and S. W. Doebling, The Statistical Sensitivity of Experimental Modal Frequencies and Damping Ratios to Measurement Noise, Internat. J. of Anal. Exp. Modal Anal. 1996, 11:63-75. AIAA, Aerospace Sciences Meeting and Exhibit, 37th, Reno, NV, Jan 11-14, 1999.
    • (1996) Internat. J. of Anal. Exp. Modal Anal , vol.11 , pp. 63-75
    • Peterson, L.D.1    Bullock, S.J.2    Doebling, S.W.3
  • 27
    • 0019609566 scopus 로고
    • An Arbitrary Lagrangian-Eulerian Finite Element Method for Transient Fluid-Structure Interactions
    • J. Donea, An Arbitrary Lagrangian-Eulerian Finite Element Method for Transient Fluid-Structure Interactions, Comput. Meths. Appl. Mech. Engrg. 1982, 33: 689-723.
    • (1982) Comput. Meths. Appl. Mech. Engrg , vol.33 , pp. 689-723
    • Donea, J.1
  • 28
    • 0029138959 scopus 로고
    • Mixed Explicit/Implicit Time Integration of Coupled Aeroelastic Problems: Three-Field Formulation, Geometric Conservation and Distributed Solution, Internat
    • C. Farhat, M. Lesoinne and N. Maman, Mixed Explicit/Implicit Time Integration of Coupled Aeroelastic Problems: Three-Field Formulation, Geometric Conservation and Distributed Solution, Internat. J. Numer. Meths. Fluids 1995, 21: 807-835.
    • (1995) J. Numer. Meths. Fluids , vol.21 , pp. 807-835
    • Farhat, C.1    Lesoinne, M.2    Maman, N.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.