Effects of flow angularity on nonlinear supersonic flutter of composite panels

Effects of flow angularity on nonlinear supersonic flutter of composite panels

Author(s):

Abdel-Motagaly, K. ( Old Dominion University )
Chen, R.
Mei, C.

Publication title:

A collection of technical papers : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, St. Louis MO, 12-15 April 1999

Title of ser.:

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

Ser. no.:

1999

Pub. Year:

1999

Vol.:

pt. 3

No.:

99-1433

Paper no.:

AIAA 99-1433

Page(from):

1963

Page(to):

1972

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563472930 [1563472937]

Language:

English

Call no.:

A07400/991201

Type:

Technical Paper

Details

TDL ID:	ZA00003932
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit
Conf. info. (Venue):	St. Louis, MO
Conf. info. (Date):	1999.04.12-1999.04.15

Similar Items:

1 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	7 Technical Paper Using Aeroelastic Modes for Nonlinear Panel Flutter At Arbitrary Supersonic Yawed Angle Mei, C., Guo, X. American Institute of Aeronautics and Astronautics
2 Technical Paper Nonlinear panel response at high acoustic excitations and supersonic speeds Abdel-Motagaly, K., Duan, B., Mei, C. American Institute of Aeronautics and Astronautics	8 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
3 Technical Paper Suppression of Supersonic Panel Flutter and Thermal Deflection Using Shape Memory Alloy Duan, B., Abdel-Motagaly, K., Guo, X., Mei, C. American Institute of Aeronautics and Astronautics	9 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
4 Technical Paper Nonlinear Flutter of Cylindrical Panels Under Yawed Supersonic Flow Using Finite Elements Azzouz, M., Mei, C. American Institute of Aeronautics and Astronautics	10 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
5 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	11 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
6 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	12 Technical Paper Three-Dimensional Nonlinear Panel Flutter at Supersonic Euler Flow Selvam, R., Qu, Z., Zheng, Q. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12