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Volumn , Issue , 1996, Pages 1124-1131

Transmission of stochastic pressures through an aeroelastic plate into a cavity

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AERODYNAMICS; AEROSPACE INDUSTRY; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; ENCLOSURES; PLATES (STRUCTURAL COMPONENTS); STOCHASTIC SYSTEMS; STRUCTURAL DYNAMICS; AIRCRAFT; MATHEMATICAL MODELS; PRESSURE; TURBULENT FLOW;

EID: 0029713238     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1445     Document Type: Conference Paper
Times cited : (4)

References (13)
  • 1
    • 0014537242 scopus 로고
    • Transmission of noise from a turbulent boundary layer through a flexible plate into a closed cavity
    • E. H. Dowell. Transmission of noise from a turbulent boundary layer through a flexible plate into a closed cavity. Journal of the Acoustical Society of America, 46(1):238-252, 1969.
    • (1969) Journal of the Acoustical Society of America , vol.46 , Issue.1 , pp. 238-252
    • Dowell, E.H.1
  • 2
    • 85003393522 scopus 로고
    • The effect of a cavity on panel vibration
    • E. H. Dowell and H. M. Voss. The effect of a cavity on panel vibration. AIAA Journal, 1(2):476-477, 1962.
    • (1962) AIAA Journal , vol.1 , Issue.2 , pp. 476-477
    • Dowell, E.H.1    Voss, H.M.2
  • 3
    • 0001174585 scopus 로고
    • The transmission of sound through a cavity-backed finite plate
    • R. W. Guy and M. C. Bhattacharya. The transmission of sound through a cavity-backed finite plate. Journal of Sound and Vibration, 27(2):207-223, 1973.
    • (1973) Journal of Sound and Vibration , vol.27 , Issue.2 , pp. 207-223
    • Guy, R.W.1    Bhattacharya, M.C.2
  • 4
    • 0029234058 scopus 로고
    • Responses of finite baffled plate to turbulent flow excitations
    • S. F. Wu and L. Maestrello. Responses of finite baffled plate to turbulent flow excitations. AIAA Journal, 33(1):13-19, 1995.
    • (1995) AIAA Journal , vol.33 , Issue.1 , pp. 13-19
    • Wu, S.F.1    Maestrello, L.2
  • 6
    • 0029224575 scopus 로고    scopus 로고
    • State space modeling for aeroelastic panels subject to full potential flow aerodynamic loading
    • New Orleans, LA, April 1995. Accepted for publication, Journal of Aircraft
    • K. D. Frampton, R. L. Clark, and E. H. Dowell. State space modeling for aeroelastic panels subject to full potential flow aerodynamic loading. In Proceedings of the 36th Structures, Structural Dynamics and Materials Conference, New Orleans, LA, pages 1183-1189, April 1995. Accepted for publication, Journal of Aircraft.
    • Proceedings of the 36Th Structures, Structural Dynamics and Materials Conference , pp. 1183-1189
    • Frampton, K.D.1    Clark, R.L.2    Dowell, E.H.3
  • 8
    • 0040167058 scopus 로고
    • Generalized aerodynamic forces on a flexible plate undergoing transient motion
    • December
    • E. H. Dowell. Generalized aerodynamic forces on a flexible plate undergoing transient motion. Quarterly of Applied Mathematics, 26(3):2267-2270, December 1967.
    • (1967) Quarterly of Applied Mathematics , vol.26 , Issue.3 , pp. 2267-2270
    • Dowell, E.H.1
  • 11
    • 0022131039 scopus 로고
    • An eigensystem realization algorithm for modal parameter identification and model reduction
    • J. Juang and R. S. Pappa. An eigensystem realization algorithm for modal parameter identification and model reduction. Journal of Guidance and Control, 8(9):620-627, 1985.
    • (1985) Journal of Guidance and Control , vol.8 , Issue.9 , pp. 620-627
    • Juang, J.1    Pappa, R.S.2
  • 12
    • 0023421592 scopus 로고
    • An error bound for a discrete reduced order model of a linear multivariable system
    • U. M. Al-Saggaf and G. F. Franklin. An error bound for a discrete reduced order model of a linear multivariable system. IEEE Transactions on Automatic Control, AC-32(9):815-819, 1987.
    • (1987) IEEE Transactions on Automatic Control , vol.AC-32 , Issue.9 , pp. 815-819
    • Al-Saggaf, U.M.1    Franklin, G.F.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.