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Volumn , Issue , 1999, Pages

Integrated aeroacoustoelastic modeling for the analysis of the propeller-driven cabin noise

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; ACOUSTIC NOISE; AEROACOUSTICS; AIRCRAFT; AVIATION; BOUNDARY INTEGRAL EQUATIONS; FUSELAGES; NOISE ABATEMENT; ORTHOGONAL FUNCTIONS; PROPELLERS; VIBRATION ANALYSIS;

EID: 84983189358     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-1919     Document Type: Conference Paper
Times cited : (5)

References (10)
  • 3
    • 0017501348 scopus 로고
    • Acoustoelasticity: General Theory, Acoustic Natural MOdes and Forced Response to Sinusoidal Excitation, Including Comparisons with Experiment
    • E.H. Dowell, G.F. Gorman III, and D. A. Smith, “Acoustoelasticity: General Theory, Acoustic Natural MOdes and Forced Response to Sinusoidal Excitation, Including Comparisons with Experiment,” Journal of Sound and Vibration, Vol. 52, No. 4, pp 519-542, 1977.
    • (1977) Journal of Sound and Vibration , vol.52 , Issue.4 , pp. 519-542
    • Dowell, E.H.1    Gorman, G.F.2    Smith, D.A.3
  • 4
    • 85025190709 scopus 로고
    • Boundary Integral Equations in Aerodynamics
    • L. Morino, “Boundary Integral Equations in Aerodynamics”, Applied Mechanics Review, Vol. 46, No. 8, pp 445-466, 1993.
    • (1993) Applied Mechanics Review , vol.46 , Issue.8 , pp. 445-466
    • Morino, L.1
  • 7
    • 84983192185 scopus 로고    scopus 로고
    • Analysis of Fuselage Vibrations Induced by the Proprotor in a Tiltrotor Aircraft
    • Williamsbutg, VA
    • M. Gennaretti and U. lemma, “Analysis of Fuselage Vibrations Induced by the Proprotor in a Tiltrotor Aircraft”, Int. I Forum on Aeroelas-ticity and Structural Dynamics, Williamsbutg, VA, June 1999.
    • (1999) Int. I Forum on Aeroelas-Ticity and Structural Dynamics
    • Gennaretti, M.1    Lemma, U.2
  • 9
    • 0043219992 scopus 로고
    • Boundary Integral Equation Methods for Aerodynamics
    • (Ed. S.N. Atluri), AIAA Progress in Aeronautics and Astronautics, AIAA, Washington, DC, 2 79321
    • L. Morino and M. Gennaretti, “Boundary Integral Equation Methods for Aerodynamics”, in Computational Nonlinear Mechanics in Aerospace Engineering (Ed.: S.N. Atluri), AIAA Progress in Aeronautics and Astronautics, Vol. 146, AIAA, Washington, DC, 2 79321, 1992.
    • (1992) Computational Nonlinear Mechanics in Aerospace Engineering , vol.146
    • Morino, L.1    Gennaretti, M.2
  • 10
    • 84983145399 scopus 로고    scopus 로고
    • Finite-State Aerodynamic Modeling for Gust Load Alleviation of Wing-Tail Configurations
    • M. Gennaretti and C. Ponzi, “Finite-State Aerodynamic Modeling for Gust Load Alleviation of Wing-Tail Configurations”, to appear in The Aeronautical Journal.
    • The Aeronautical Journal
    • Gennaretti, M.1    Ponzi, C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.