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Volumn 43, Issue 3, 2006, Pages 763-772

Unified aeroelastic and flight dynamic formulation via rational function approximations

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; APPROXIMATION THEORY; CONTROL SYSTEMS; DEGREES OF FREEDOM (MECHANICS); DRAG; EQUATIONS OF MOTION; FLIGHT DYNAMICS; PERTURBATION TECHNIQUES;

EID: 33746133153     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.16620     Document Type: Article
Times cited : (51)

References (16)
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    • Rodden, W.P.1    Love, J.R.2
  • 4
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    • Reduced order dynamic aeroelastic model development and integration with nonlinear simulation
    • Winther, B. A., Goggin, P. J., and Dykman, J. R., "Reduced Order Dynamic Aeroelastic Model Development and Integration with Nonlinear Simulation," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 833-839.
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    • Winther, B.A.1    Goggin, P.J.2    Dykman, J.R.3
  • 5
    • 0033726730 scopus 로고    scopus 로고
    • Structural dynamics and quasistatic aeroelastic equations of motion
    • Dykman, J. R., and Rodden, W., "Structural Dynamics and Quasistatic Aeroelastic Equations of Motion," Journal of Aircraft, Vol. 37, No. 3, 2000, pp. 538-542.
    • (2000) Journal of Aircraft , vol.37 , Issue.3 , pp. 538-542
    • Dykman, J.R.1    Rodden, W.2
  • 6
    • 33746121960 scopus 로고
    • Errata and addenda to 'application of oscillatory aerodynamic theory to estimation of dynamic stability derivatives
    • Rodden, W. P., Bellinger, E. D., and Giesing, J. P., "Errata and Addenda to 'Application of Oscillatory Aerodynamic Theory to Estimation of Dynamic Stability Derivatives,'" Journal of Aircraft, Vol. 21, No. 1, 1984, pp. 93, 94.
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    • Rodden, W.P.1    Bellinger, E.D.2    Giesing, J.P.3
  • 8
    • 33746141322 scopus 로고    scopus 로고
    • Aeroelastic analysis of a composite unmanned air vehicle
    • April
    • Kosmatka, J. B., and Panza, J., "Aeroelastic Analysis of a Composite Unmanned Air Vehicle," AIAA Paper 2002-1208, April 2002.
    • (2002) AIAA Paper , vol.2002 , Issue.1208
    • Kosmatka, J.B.1    Panza, J.2
  • 9
  • 10
    • 85007667458 scopus 로고
    • Size-reduction techniques for the determination of efficient aeroservoelastic models
    • Academic Press, San Diego, CA
    • Karpel, M., "Size-Reduction Techniques for the Determination of Efficient Aeroservoelastic Models," Control and Dynamic Systems-Advances In Theory and Applications, Vol. 54, Academic Press, San Diego, CA, 1992, pp. 263-295.
    • (1992) Control and Dynamic Systems-Advances in Theory and Applications , vol.54 , pp. 263-295
    • Karpel, M.1
  • 13
    • 0020098320 scopus 로고
    • Design of the active flutter suppression and gust load alleviation using state-space aeroelastic modeling
    • Karpel, M., "Design of the Active Flutter Suppression and Gust Load Alleviation Using State-Space Aeroelastic Modeling," Journal of Aircraft, Vol. 19, No. 6, 1982, pp. 221-227.
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    • Karpel, M.1
  • 14
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    • A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flow
    • Albano, E., and Rodden, W. P., "A Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flow," AIAA Journal, Vol. 7, No. 2, 1969, pp. 279-285.
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    • Albano, E.1    Rodden, W.P.2
  • 15
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    • Wolfram Media, Champaign, IL
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    • Wolfram, S.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.