Modeling Cylinder Flow Vortex Shedding with Enforced Motion Using a Harmonic Balance Approach

Modeling Cylinder Flow Vortex Shedding with Enforced Motion Using a Harmonic Balance Approach

Author(s):

M. Spiker ( Duke University, Durham, NC )
J. Thomas
K. Hall
R. Kielb
E. Dowell

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.:

2006-1965

Paper no.:

AIAA Paper 2006-1965

Pub. info.:

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

ISSN:

10877215

Language:

English

Call no.:

A07400/200607 [CD-ROM 2006 Disc 7]

Type:

Technical Paper

Details

TDL ID:	ZA00047226
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 A Harmonic Balance Approach for Modeling Nonlinear Aeroelastic Behavior of Wings in Transonic Viscous Flow Thomas, J., Hall, K., Dowell, E. American Institute of Aeronautics and Astronautics	7 Technical Paper Computational Models for Nonlinear Aeroelasticity Carlson, H., Feng, J., Dowell, E., Thomas, J., Hall, K., Kielb, R. American Institute of Aeronautics and Astronautics
2 Technical Paper Modeling Viscous Transonic Limit Cycle Oscillation Behavior Using a Harmonic Balance Approach Thomas, J., Dowell, E., Hall, K. American Institute of Aeronautics and Astronautics	8 Technical Paper Harmonic Balance Analysis of Forced Response in a Transonic Compressor K. Ekici, K. Hall, R. Kielb American Institute of Aeronautics and Astronautics
3 Technical Paper Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach Thomas, J., Dowell, E., Hall, K., Denegri, C. American Institute of Aeronautics and Astronautics	9 Technical Paper Transonic Limit Cycle Oscillation Analysis Using Reduced Order Aerodynamic Models Dowell,E., Thomas,J., Hall,K. American Institute of Aeronautics and Astronautics
4 Technical Paper Further Invesitgation of Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach Thomas, J., Dowell, E., Hall, K., Denegri, C. American Institute of Aeronautics and Astronautics	10 Technical Paper Using Automatic Differentiation to Create a Nonlinear Reduced Order Model Aeroelastic Solver J. Thomas, E. Dowell, K. Hall American Institute of Aeronautics and Astronautics
5 Technical Paper Application of Enforced Motion to Study 2-D Cascade Lock-in Effect M. Spiker, R. Kielb, J. Thomas, K. Hall American Institute of Aeronautics and Astronautics	11 Technical Paper Three-Dimensional Transonic Aeroelasticity Using Proper Orthogonal Depcomposition Based Reduced Order Models Thomas,J., Dowell,E., Hall,K. American Institute of Aeronautics and Astronautics
6 Technical Paper Efficient Design Method for Non-Synchronous Vibrations Using Enforced Motion. Spiker, M.A., Kield, R.E., Hall, K.C., Thomas, J.P. American Society of Mechanical Engineers	12 Technical Paper Using Automatic Differentiation to Create a Nonlinear Reduced Order Model of a Computational Fluid Dynamic Solver J. Thomas, E. Dowell, K. Hall American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12