Sound Transmission Through a Curved Honeycomb Composite Panel

Sound Transmission Through a Curved Honeycomb Composite Panel

Author(s):

Publication title:

A collection of technical papers : 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, Hilton Head, South Carolina, 12-14 May 2003

Title of ser.:

AIAA Paper : AIAA/CEAS Aeroacoustics Conference

Ser. no.:

2003

Pub. Year:

2003

Vol.:

v. 1

No.:

2003-3157

Paper no.:

AIAA-2003-3157

Page(from):

517

Page(to):

525

Pages:

9

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISBN:

9781563475979 [1563475979]

Language:

English

Call no.:

A07400/033100 (v.1)

Type:

Technical Paper

Details

TDL ID:	ZA00001576
Series ID:	PA00000149
Conf. info. (Name):	AIAA/CEAS Aeroacoustics Conference and Exhibit
Conf. info. (Number):	9th
Conf. info. (Venue):	Hilton Head, South Carolina
Conf. info. (Date):	2003.05.12-2003.05.14

Similar Items:

1 Technical Paper Radiated Sound Power from a Curved Honeycomb Panel Robinson, J., Buehrle, R., Klos, J., Grosveld, F. American Institute of Aeronautics and Astronautics	7 Technical Paper Energy Finite Element Analysis of the NASA Aluminum Testbed Cylinder. Wang, A., Vlahopoulos, N., Buehrle, R.D., Klos, J. Society of Automotive Engineers
2 Technical Paper Vibroacoustic Model Validation for a Curved Honeycomb Composite Panel Buehrle,R., Robinson,J., Grosveld,F. American Institute of Aeronautics and Astronautics	8 Technical Paper Effect of Damping on Sound Transmission Loss Through Automotive Body Panels. Patil, A.R., Goetchius, G.M. Society of Automotive Engineers
3 Technical Paper Structural and Acoustic Numerical Modeling of a Curved Composite Honeycomb Panel Grosveld,F., Buehrle,R., Robinson,J. American Institute of Aeronautics and Astronautics	9 Technical Paper Sound transmission through cylindrical shell structures excited by boundary layer pressure fluctuations Tang, Yvette Y., Silcox, Richard J., Robinson, Jay H. American Institute of Aeronautics and Astronautics
4 Technical Paper Sound transmission through a cylindrical sandwich shell with honeycomb core Tang, Yvette Y., Robinson, Jay H., Silcox, Richard J. American Institute of Aeronautics and Astronautics	10 Technical Paper Acoustic Source Localization in Aircraft Interiors Using Microphone Array Technologies B. Sklanka, J. Tuss, R. Buehrle, J. Klos, E. Williams, N. Valdivia American Institute of Aeronautics and Astronautics
5 Technical Paper Noise Transmission Characteristics of Damped Plexiglas Windows Gibbs, G., Buehrle, R., Klos, J., Brown, S. American Institute of Aeronautics and Astronautics	11 Technical Paper Active control of structure-borne and air-borne sound transmission through a double panel Gardonio, P., Elliott, S.J. American Institute of Aeronautics and Astronautics
6 Technical Paper Modeling and Validation of Damped Plexiglas Windows for Noise Control Buehrle, R., Gibbs, G., Klos, J., Mazur, M. American Institute of Aeronautics and Astronautics	12 Technical Paper A STUDY OF METHODS TO PREDICT AND MEASURE THE TRANSMISSION OF SOUND THROUGH THE WALLS OF LIGHT AIRCRAFT Bernhard, R.J. et al. National Aeronautics and Space Administration

1

2

3

4

5

6

7

8

9

10

11

12