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Volumn , Issue , 2004, Pages 2079-2090

Quantification of aircraft non-linearities from flight flutter test data

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AUTOMATION; CONTROL SYSTEMS; DAMPING; EQUATIONS OF MOTION; FREQUENCIES; HARMONIC ANALYSIS; NONLINEAR SYSTEMS; OSCILLATIONS; STIFFNESS;

EID: 13344282696     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (3)

References (13)
  • 3
    • 0346294152 scopus 로고    scopus 로고
    • F/A-18 a flight flutter testing - Limit cycle oscillation or flutter?
    • S.Dunne, F/A-18 A Flight Flutter Testing - Limit Cycle Oscillation or Flutter ?, Int Forum on Aeroelasticity and Structural Dynamics (2001) pp193-204
    • (2001) Int Forum on Aeroelasticity and Structural Dynamics , pp. 193-204
    • Dunne, S.1
  • 4
    • 0006746518 scopus 로고    scopus 로고
    • A new compendium of unsteady aerodynamic test cases for CFD: Summary of AVT WG-003 activities
    • L.P. Ruiz-Calavera et al, A New Compendium of Unsteady Aerodynamic Test Cases for CFD: Summary of AVT WG-003 Activities. Int Forum on Aeroelasticity and Structural Dynamics (1999) pp1-11.
    • (1999) Int Forum on Aeroelasticity and Structural Dynamics , pp. 1-11
    • Ruiz-Calavera, L.P.1
  • 5
    • 10844264205 scopus 로고    scopus 로고
    • Limit cycle oscillation prediction for non-linear aeroelastic systems
    • A. Sedaghat et al. Limit Cycle Oscillation Prediction for Non-Linear Aeroelastic Systems, Aeronautical Journal v106 n1056 (2002) pp27-32
    • (2002) Aeronautical Journal , vol.106 , Issue.1056 , pp. 27-32
    • Sedaghat, A.1
  • 7
    • 3943071119 scopus 로고    scopus 로고
    • Identification of multi-degree of freedom systems with non-proportional damping using the resonant decay method
    • S. Naylor, M.F. Platten, J R Wright & J.E. Cooper, Identification of Multi-Degree of Freedom Systems with Non-Proportional Damping using the Resonant Decay Method, J.Vibration and Acoustics v126 (2004) pp298-306.
    • (2004) J.Vibration and Acoustics , vol.126 , pp. 298-306
    • Naylor, S.1    Platten, M.F.2    Wright, J.R.3    Cooper, J.E.4
  • 10
    • 0038343470 scopus 로고    scopus 로고
    • Time-frequency analysis of non-linear systems: The skeleton linear model and the skeleton curves
    • ASME
    • L. Wang, J. Zhang, C. Wang, S. Hu, Time-Frequency Analysis of Non-linear Systems: The Skeleton Linear Model and the Skeleton Curves, Journal of Vibration and Acoustics, Vol. 125, ASME (2003), pp. 170-177.
    • (2003) Journal of Vibration and Acoustics , vol.125 , pp. 170-177
    • Wang, L.1    Zhang, J.2    Wang, C.3    Hu, S.4
  • 11
    • 0000753008 scopus 로고
    • Non-linear system vibration analysis using Hilbert transform - I. Free vibration analysis method 'FREEVIB'
    • Academic Press
    • M. Feldman, Non-Linear System Vibration Analysis using Hilbert Transform - I. Free Vibration Analysis Method 'FREEVIB', Mechanical Systems and Signal Processing, Vol. 8, No. 2, Academic Press (1994), pp. 119-127.
    • (1994) Mechanical Systems and Signal Processing , vol.8 , Issue.2 , pp. 119-127
    • Feldman, M.1
  • 12
    • 0032121362 scopus 로고    scopus 로고
    • Identification on non -linear systems using multi-scale ridges and skeletons of the wavelet transform
    • Academic Press
    • W. J. Staszewski, Identification on Non -Linear Systems using Multi-Scale Ridges and Skeletons of the Wavelet Transform, Journal of Sound and Vibration, Vol. 214, No. 4, Academic Press (1998), pp. 639-658.
    • (1998) Journal of Sound and Vibration , vol.214 , Issue.4 , pp. 639-658
    • Staszewski, W.J.1
  • 13
    • 0027660898 scopus 로고
    • Envelope function - A tool for analyzing flutter data
    • AIAA
    • J. E. Cooper, P. R. Emmett, J. R. Wright, M. J. Schofield, Envelope Function - A Tool for Analyzing Flutter Data, Journal of Aircraft, Vol. 30, No. 5, AIAA (1993), pp. 785-790.
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 785-790
    • Cooper, J.E.1    Emmett, P.R.2    Wright, J.R.3    Schofield, M.J.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.