메뉴 건너뛰기




Volumn 21, Issue 3 SPEC. ISS., 2005, Pages 243-255

Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight

Author keywords

Reduced order models; Transonic flows; Wing aeroelasticity

Indexed keywords

BOUNDARY ELEMENT METHOD; EIGENVALUES AND EIGENFUNCTIONS; INTEGRAL EQUATIONS; MATHEMATICAL MODELS; MATRIX ALGEBRA; POTENTIAL FLOW; STATE SPACE METHODS; TIME DOMAIN ANALYSIS; TRANSFER FUNCTIONS; TRANSONIC FLOW; UNSTEADY FLOW; WINGS;

EID: 27744530077     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2005.05.014     Document Type: Article
Times cited : (10)

References (15)
  • 1
    • 0242342202 scopus 로고
    • An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics
    • NASA Technical Memorandum X-79
    • R.V. Doggett A.G. Rainey H.G. Morgan An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics NASA Technical Memorandum X-79 1959
    • (1959)
    • Doggett, R.V.1    Rainey, A.G.2    Morgan, H.G.3
  • 2
    • 0242342209 scopus 로고
    • A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils
    • NASA Contract Report 82-3537
    • Ehlers, S.E., Weatherill, W.H., 1982. A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils. NASA Contract Report 82-3537.
    • (1982)
    • Ehlers, S.E.1    Weatherill, W.H.2
  • 4
    • 0017998869 scopus 로고
    • Small unsteady perturbations in transonic flows
    • K.Y. Fung N.J. Yu R. Seebass Small unsteady perturbations in transonic flows AIAA Journal 16 1978 815-822
    • (1978) AIAA Journal , vol.16 , pp. 815-822
    • Fung, K.Y.1    Yu, N.J.2    Seebass, R.3
  • 5
    • 2342450567 scopus 로고    scopus 로고
    • Study of reduced-order models for gust-response analysis of flexible wings
    • M. Gennaretti F. Mastroddi Study of reduced-order models for gust-response analysis of flexible wings Journal of Aircraft 41 2004 304-313
    • (2004) Journal of Aircraft , vol.41 , pp. 304-313
    • Gennaretti, M.1    Mastroddi, F.2
  • 6
    • 0032669102 scopus 로고    scopus 로고
    • Finite-state aerodynamic modelling for gust load alleviation of wing-tail configurations
    • M. Gennaretti C. Ponzi Finite-state aerodynamic modelling for gust load alleviation of wing-tail configurations The Aeronautical Journal 103 1999 147-158
    • (1999) The Aeronautical Journal , vol.103 , pp. 147-158
    • Gennaretti, M.1    Ponzi, C.2
  • 7
    • 27744453684 scopus 로고    scopus 로고
    • A comparison among some aeroelastic models for the stability analysis of a flap-lag-torsion helicopter rotor in hover
    • 26th European Rotorcraft Forum, The Hague, The Netherlands
    • Gennaretti, M., Corbelli, A., Mastroddi, F., 2000. A comparison among some aeroelastic models for the stability analysis of a flap-lag-torsion helicopter rotor in hover. 26th European Rotorcraft Forum, The Hague, The Netherlands.
    • (2000)
    • Gennaretti, M.1    Corbelli, A.2    Mastroddi, F.3
  • 9
    • 27744560786 scopus 로고
    • Comparison between computations and experimental data in unsteady three-dimensional transonic aerodynamics, including aeroelastic applications
    • NASA Technical Note 82-06090
    • Guruswamy, G.P., Goorjian, P.M., 1982. Comparison between computations and experimental data in unsteady three-dimensional transonic aerodynamics, including aeroelastic applications. NASA Technical Note 82-06090.
    • (1982)
    • Guruswamy, G.P.1    Goorjian, P.M.2
  • 10
    • 0039415396 scopus 로고    scopus 로고
    • Steady two-dimensional analysis using a boundary integral equation method
    • U. Iemma L. Morino Steady two-dimensional analysis using a boundary integral equation method Journal of Fluids and Structures 11 1997 247-269
    • (1997) Journal of Fluids and Structures , vol.11 , pp. 247-269
    • Iemma, U.1    Morino, L.2
  • 11
    • 0005038833 scopus 로고
    • Transonic potential flow calculation using conservation form
    • Hartford, Connecticut, USA
    • Jameson, A., 1975. Transonic potential flow calculation using conservation form. AIAA Second Computational Fluid Dynamics Proceedings, Hartford, Connecticut, USA, pp. 148-161.
    • (1975) AIAA Second Computational Fluid Dynamics Proceedings , pp. 148-161
    • Jameson, A.1
  • 13
    • 0027696264 scopus 로고
    • Boundary integral equations and conservative dissipation schemes for full-potential transonic flow
    • L. Morino U. Iemma Boundary integral equations and conservative dissipation schemes for full-potential transonic flow Computational Mechanics 13 1993 90-100
    • (1993) Computational Mechanics , vol.13 , pp. 90-100
    • Morino, L.1    Iemma, U.2
  • 14
    • 3042826212 scopus 로고    scopus 로고
    • Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 code
    • W.A. Silva R.E. Bartels Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 code Journal of Fluids and Structures 19 2004 729-745
    • (2004) Journal of Fluids and Structures , vol.19 , pp. 729-745
    • Silva, W.A.1    Bartels, R.E.2
  • 15
    • 0018453051 scopus 로고
    • The linearization of transonic flows containing shocks
    • M.H. Williams The linearization of transonic flows containing shocks AIAA Journal 17 1979 394-397
    • (1979) AIAA Journal , vol.17 , pp. 394-397
    • Williams, M.H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.