Time Domain Method for Nonlinear Flutter of Curved Panels Under Yawed Supersonic Flow at Elevated Temperature

Time Domain Method for Nonlinear Flutter of Curved Panels Under Yawed Supersonic Flow at Elevated Temperature

Author(s):

Ghoman, Satyajit ( Virginia Polytechnic Institute and State University, Blacksburg, VA, 24061 )
Azzouz, Mohammed ( Midwestern State University, Wichita Falls, TX, 76308 )
Mei, Chuh ( Old Dominion University, Norfolk, VA, 23529 )

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.:

2009

Pub. Year:

2009

No.:

2009-2598

Paper no.:

AIAA Paper 2009-2598

Pages:

11

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200905

Type:

Technical Paper

Link(DOI, etc.)

http://doi.org/10.2514/6.2009-2598

Details

TDL ID:	ZA00066595
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Conf. info. (Number):	50th
Conf. info. (Venue):	Palm Springs, California
Conf. info. (Date):	2009.05.04-2009.05.07
Note for article:	50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 17th 4-7 May 2009, Palm Springs, California

Similar Items:

1 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	7 Technical Paper Flow Angle Effects on Supersonic Flutter of Clamped Curved Panels Azzouz, Mohamed American Institute of Aeronautics and Astronautics
2 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	8 Technical Paper Using Aeroelastic Modes for Nonlinear Panel Flutter At Arbitrary Supersonic Yawed Angle Mei, C., Guo, X. American Institute of Aeronautics and Astronautics
3 Technical Paper Nonlinear Flutter of Cylindrical Panels Under Yawed Supersonic Flow Using Finite Elements Azzouz, M., Mei, C. American Institute of Aeronautics and Astronautics	9 Technical Paper Pre-Flutter Modes Analysis of Curved Panels Using Nonlinear Finite Elements M. Azzouz American Institute of Aeronautics and Astronautics
4 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	10 Technical Paper An equivalent linearization/double transformation method for nonlinear random composite panel response Chen, Roger, Mei, Chuh American Institute of Aeronautics and Astronautics
5 Technical Paper Finite Element Time Domain - Modal Formulation for Nonlinear Flutter of Composite Curved Panels M. Azzouz, C. Mei American Institute of Aeronautics and Astronautics	11 Technical Paper Flow Angle, Temperature and Aerodynamic Damping on Supersonic Panel Flutter Stability Boundary Mei, C., Lee, Y., Cheng, G. American Institute of Aeronautics and Astronautics
6 Technical Paper Active Control of Nonlinear Panel Flutter Under Yawed Supersonic Flow Abdel-Motagaly, K., Duan, B., 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