Using Automatic Differentiation to Create a Nonlinear Reduced Order Model Aeroelastic Solver

Using Automatic Differentiation to Create a Nonlinear Reduced Order Model Aeroelastic Solver

Author(s):

J. Thomas ( Duke University, Durham, NC )
E. Dowell
K. Hall

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.:

2008

Pub. Year:

2008

No.:

2008-2322

Paper no.:

AIAA Paper 2008-2322

Pub. info.:

Reno, Nevada: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200803 [CD-ROM 2008 Disc 3]

Type:

Technical Paper

Details

TDL ID:	ZA00049521
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Conf. info. (Number):	49th
Conf. info. (Venue):	Schaumburg, IL
Conf. info. (Date):	2008.04.07-2008.04.10
Note for article:	49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 7-10 April 2008, Schaumburg, IL

Similar Items:

1 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	7 Technical Paper Reduced-order modelling of unsteady small-disturbance flows using a frequency-domain proper orthogonal decomposition technique Hall, K.C., Thomas, J.P., Dowell, E.H. American Institute of Aeronautics and Astronautics
2 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	8 Technical Paper Modeling Limit Cycle Oscillations for an NLR 7301 Airfoil Aeroelastic Configuration Including Correlation with Experiment Thomas, J., Dowell, E., Hall, K. American Institute of Aeronautics and Astronautics
3 Technical Paper Transonic Limit Cycle Oscillation Analysis Using Reduced Order Aerodynamic Models Dowell,E., Thomas,J., Hall,K. American Institute of Aeronautics and Astronautics	9 Technical Paper An Efficient Approach for Solving Nonlinear Aeroelastic Phenomenona Using Reduced-Order Modeling Munteanu, S., Rajadas, J., Nam, C., Chathopadhyay, A. American Institute of Aeronautics and Astronautics
4 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	10 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
5 Technical Paper Reduced-Order Modelling of Unsteady Small-Disturbance Flows Using a Frequency-Domain Proper Orthogonal Decomposition Technique Hall, K. C., Thomas, J. P., Dowell, E. H. American Institute of Aeronautics and Astronautics	11 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
6 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	12 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

1

2

3

4

5

6

7

8

9

10

11

12