Using Aeroelastic Modes for Nonlinear Panel Flutter At Arbitrary Supersonic Yawed Angle

Using Aeroelastic Modes for Nonlinear Panel Flutter At Arbitrary Supersonic Yawed Angle

Author(s):

Publication title:

A collection of technical papers : 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference : 10th AIAA/ASME/AHS Adaptive Structures Forum : 4th AIAA Non-Deterministic Approaches Forum : 3rd AIAA Gossamer Spacecraft Forum, Denver, Colorado, 22-25 April 2002

Title of ser.:

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

Ser. no.:

2002

Pub. Year:

2002

Vol.:

v. 4

No.:

2002-1486

Paper no.:

AIAA-2002-1486

Page(from):

2277

Page(to):

2286

Pages:

10

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563475429 [1563475421]

Language:

English

Call no.:

A07400/021200 (v.4)

Type:

Technical Paper

Details

TDL ID:	ZA00001445
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; AIAA/ASME/AHS Adaptive Structures Forum ; AIAA Non-Deterministic Approaches Forum ; AIAA Gossamer Spacecraft Forum
Conf. info. (Number):	43rd ; 10th ; 4th ; 3rd
Conf. info. (Venue):	Denver, Colorado
Conf. info. (Date):	2002.04.22-2002.04.25

Similar Items:

1 Technical Paper Supersonic Panel Flutter Analysis and Suppression Using Aeroelastic Modes and Shape Memory Alloys Guo, X., Przekop, A., Mei, C. American Institute of Aeronautics and Astronautics	7 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
2 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	8 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
3 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	9 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
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 Effects of flow angularity on nonlinear supersonic flutter of composite panels Abdel-Motagaly, K., Chen, R., Mei, C. American Institute of Aeronautics and Astronautics
5 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	11 Technical Paper Nonlinear Random Response of Shallow Shells at Elevated Temperatures Using Finite Element Modal Method Guo, X., Mei, C., Przekop, A. 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 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

1

2

3

4

5

6

7

8

9

10

11

12