The prediction of structural noise induced vibration

S V Sound and Vibration

Volumn 30, Issue 4, 1996, Pages 30-34

  Vallance, Charles ^a   Vlahopoulos, Nickolas ^b  

^a AEROJET ROCKETDYNE   (United States)

^b Automated Analysis Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AEROSPACE APPLICATIONS; BOUNDARY ELEMENT METHOD; DYNAMIC RESPONSE; FINITE ELEMENT METHOD; GREEN'S FUNCTION; INTEGRAL EQUATIONS; MATHEMATICAL MODELS; NUMERICAL ANALYSIS; STATISTICAL METHODS; VECTORS; VIBRATIONS (MECHANICAL);

HELMHOLTZ INTEGRAL EQUATION; NOISE INDUCED VIBRATION; OVERALL SOUND PRESSURE LEVEL; STRUCTURAL NOISE;

STRUCTURAL ANALYSIS;

EID: 0030123207     PISSN: 00381810     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (16)

1. Burton, A. J., and Miller, G. F., "The Application of Integral Equation Methods to the Numerical Solutions of Some Exterior Boundary Value Problems," Proc. Roy. Soc. London, Vol. 323, pp. 201-210, 1971.
2. COMET/Acoustics, User Document, Ver. 2.1, July 1994, Automated Analysis Corporation, Ann Arbor, MI.
3. Foss, R. L. and Kacena, W. J., "On Combining Finite Element Modeling and Lower Level Measured Responses to Predict Deformation of a Structure Subjected to Reverberant Acoustic Excitation," 65th Shock and Vibration Bulletin, (1994).
4. Hamdi, M. A., "Formulation Variationnelle Par Equations Integrales pour le Calcul de Champs Acoustiques Lineaires Proches et Lointaines," These d' Etat, Universite de Compiegne, 1982.
5. Imai, M., Suzuki, S., Sugiura, N., and Sato, H., "Radiation Efficiency of Engine Structures, Analyzed by Holographic Interferometry and Boundary Element Calculation," SAE Paper 861411, 1986.
6. Kennedy, M., "Titan 15:1 Skirt/Closure Assembly Structural Analysis Due to the TYPE II Flight Acoustic Environment," Aerojet Internal Memo 5235:4921, dated 4 November 1992.
7. Koopman, G. H., and Benner, H., "Method for Computing the Sound Power of Machines Based on the Helmholtz Integral," Journal of Acous. Soc. Am., Vol. 71, pp. 77-89, 1982.
8. Lieberman, P., Bocksrucker, R., Pilgram, Vallance, C., "Progressive Wave Tube Facility with Additional Capabilities," AIAA 93-0288, presented at the 31st Aerospace Sciences Meeting and Exhibit, January 1993.
9. Nefske, D. J., Wolf, J. A., and Howell, L.J., "Structural - Acoustic Analysis Using Finite Element Methods," Chapter 11 of Modern Automotive Structural Analysis.
10. Seybert, A. F., Soenarko, B., Rizzo, F. J., and Shippy, D. J., "Application of the BIE Method to Sound Radiation Problems Using an Isoparametric Element," ASME transactions, J. Vib. Acous. Stress Rel. Dsgn., Vol. 106, pp. 414-420, 1984.
11. Smith, D. C., "Noise Control Design of Vibrating Structures Using the Boundary Element Method," MS Thesis, Purdue University, 1988.
12. Smith, D. C., and Bernhard, R. J., "An Experimental Verification of Numerical Techniques Based on the Helmholtz and Rayleigh Integral Equations," Noise-Con 88, Purdue University, pp. 615-620, 1988.
13. Suzuki, S., Maruyama, S., and Ido, H., "Boundary Element Analysis of Cavity Noise Problems with Complicated Boundary Conditions," Journal of Sound and Vibration, vol. 130, pp. 79-91, 1989.
14. Utsumo, H., Tanaka, T., Inoue, K., and Nishibe, M., "Analysis of the Sound Field in an Automotive Cabin by Using Boundary Element Method," SAE Paper 891153, 1989.
15. Vallance, C. S., "Titan IV Turbine Exhaust Nozzle Modification Acoustic Test and Analysis," Aerojet Internal Memo 5276:5095, dated 27 September 1994.
16. Vlahopoulos, N., Shalis, E. V., and Latcha, M. A., "A Numerical Approach for the Prediction and Reduction of Structure-Borne Noise During the Design Stage of Ground Vehicles," 14th ASME Biennial Conference on Mechanical Vibration and Noise, Albuquerque, New Mexico, pp. 73-80, 1993.