Three-Dimensional Transonic Aeroelasticity Using Proper Orthogonal Depcomposition Based Reduced Order Models

Three-Dimensional Transonic Aeroelasticity Using Proper Orthogonal Depcomposition Based Reduced Order Models

著者名:

掲載資料名:

A collection of technical papers : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit : AIAA/ASME/ASCE/AHS Adaptive Structures Forum : AIAA Non-Deterministic Approaches Forum : AIAA Gossamer Spacecraft Forum, Seattle, Washington, 16-19 April 2001

シリーズ名:

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

シリーズ巻号:

2001

発行年:

2001

巻:

v. 4

通号:

2001-1526

ペーパー番号:

AIAA-2001-1526

開始ページ:

2555

終了ページ:

2564

総ページ数:

10

出版情報:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563474774 [1563474778]

言語:

英語

請求記号:

A07400/011180

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00000081
シリーズID:	PA00000154
会議名:	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit ; AIAA/ASME/ASCE/AHS Adaptive Structures Forum ; AIAA Non-Deterministic Approaches Forum ; AIAA Gossamer Spacecraft Forum
会議開催地:	Seattle, Washington
会議開催年:	2001.04.16-2001.04.19

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1 テクニカルペーパー 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	7 テクニカルペーパー 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
2 テクニカルペーパー Using Automatic Differentiation to Create a Nonlinear Reduced Order Model Aeroelastic Solver J. Thomas, E. Dowell, K. Hall American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Modeling Viscous Transonic Limit Cycle Oscillation Behavior Using a Harmonic Balance Approach Thomas, J., Dowell, E., Hall, K. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Transonic Limit Cycle Oscillation Analysis Using Reduced Order Aerodynamic Models Dowell,E., Thomas,J., Hall,K. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー 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
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