Finite Element Time Domain - Modal Formulation for Nonlinear Flutter of Composite Curved Panels

Finite Element Time Domain - Modal Formulation for Nonlinear Flutter of Composite Curved Panels

Author(s):

M. Azzouz ( Old Dominion University, Norfolk, VA )
C. Mei

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-1732

Paper no.:

AIAA Paper 2006-1732

Pub. info.:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200606 [CD-ROM 2006 Disc 6]

Type:

Technical Paper

Details

TDL ID:	ZA00047225
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; AIAA/ASME/AHS Adaptive Structures Conference
Conf. info. (Number):	47th ; 14th
Conf. info. (Venue):	Newport, Rhode Island
Conf. info. (Date):	2006.05.01-2006.05.04

Similar Items:

1 Technical Paper Nonlinear Flutter of Curved Panels Under Yawed Supersonic Flow Using Finite Elements Azzouz, M., Przekop, A., Guo, X., Mei, C. American Institute of Aeronautics and Astronautics	7 Technical Paper Reinvestigation of Nonlinear Random Response of Shallow Shells Using Finite Element Modal Formulation Przekop, A., Guo, X., Azzouz, S., Mei, C. American Institute of Aeronautics and Astronautics
2 Technical Paper Nonlinear Flutter of Cylindrical Panels Under Yawed Supersonic Flow Using Finite Elements Azzouz, M., Mei, C. American Institute of Aeronautics and Astronautics	8 Technical Paper Nonlinear Flutter of Cylindrical Shell Panels Under Yawed Supersonic Flow Using FE Azzouz, M., Guo, X., Przekop, A., Mei, C. American Institute of Aeronautics and Astronautics
3 Technical Paper Time Domain Method for Nonlinear Flutter of Curved Panels Under Yawed Supersonic Flow at Elevated Temperature Ghoman, Satyajit, Azzouz, Mohammed, Mei, Chuh American Institute of Aeronautics and Astronautics	9 Technical Paper Nonlinear Stiffness Estimation for Modal Finite Element Approach to Free Vibrations of Shallow Shells Przekop, A., Azzouz, S., Guo, X., Mei, C., Azrar, L. American Institute of Aeronautics and Astronautics
4 Technical Paper Pre-Flutter Modes Analysis of Curved Panels Using Nonlinear Finite Elements M. Azzouz American Institute of Aeronautics and Astronautics	10 Technical Paper Nonlinear Response and Fatigue Life of Shallow Shells to Acoustic Excitation Using Finite Element Przekop, A., Guo, X., Azzouz, S., Mei, C. American Institute of Aeronautics and Astronautics
5 Technical Paper Frequency Domain Method for Flutter of Curved Panels Under Yawed Supersonic Flow at Elevated Temperatures S. Ghoman, C. Mei, M. Azzouz American Institute of Aeronautics and Astronautics	11 Technical Paper Large amplitude free vibrations of composite plates using the finite element time domain - modal method Shi, Yucheng, Lee, Raymond Y.Y., Mei, Chuh American Institute of Aeronautics and Astronautics
6 Technical Paper Finite Element Modal Formulation for Hypersonic Panel Flutter Analysis with Thermal Effects Cheng, G., Mei, C. American Institute of Aeronautics and Astronautics	12 Technical Paper Effects of flow angularity on nonlinear supersonic flutter of composite panels Abdel-Motagaly, K., Chen, R., Mei, C. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12