The nonlinear acoustic response of thermally buckled plates

Applied Acoustics

Volumn 59, Issue 3, 2000, Pages 237-251

  Ng, C F ^a  

^a HONG KONG POLYTECHNIC UNIVERSITY   (Hong Kong)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0011780553     PISSN: 0003682X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0003-682X(99)00009-2     Document Type: Article

References (12)

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3. Moorthy L, Mei C, Shirahatti U. Numerical simulation of acoustically induced nonlinear variations of a plate with temperature gradient. 36th Structures, Structural Dynamics, and Materials Conference. AIAA-95-1378-CP, New Orleans, LA, Apr. 10-13, 1995. p. 1844-54.
4. Lee J. Large-amplitude plate vibration in an elevated thermal environment. Appl Mech Rev 1993;46:S242-S254.
5. Souza MA, Mook DT. Post-buckling nonlinear vibrations of initially imperfect structural systems. 32nd Structures, Structural Dynamics, and Materials Conference, AIAA-91-1228-CP, Baltimore, MD, 1991.p. 2772-5.
6. Shi Y, Mei CC. Chaotic structural acoustic response of a milled aluminum panel. 36th Structures, Structural Dynamics, and Materials Conference. AIAA-95-1301-CP, New Orleans, LA, Apr. 10-13, 1995. p. 1240-1250.
7. Leatherwood D, Clevenson S, Powell CA. Acoustic testing of high-temperature panels. J Aircraft 1992; 29(6).
8. Ng CF. The comparison of theoretical and experimental results of nonlinear random of composite plates. Composite Structures 1998; in press.
9. Ng CF. Design guide for predicting nonlinear random response NASA Contract Report. CR-181877, Sept., 1989.
10. Ng CF. Testing techniques for chaotic vibration of buckled aircraft structures. Proc. Institute of Mechanical Engineers Pt. G.J. Aerospace Engineering 1996;210:281-90.
11. Ng CF. Nonlinear and snap-through responses of curved panels to Intense Acoustic Excitation. Journal of Aircraft 1989;26(3):281-8.
12. Ng CF, Clevenson S. High intensity acoustic tests of a thermally stressed aluminum plate in TAFA. NASA-TMA01 552, Feb., 1989.