Higher Order Harmonic Balance Analysis for Limit Cycle Oscillations in an Airfoil with Cubic Restoring Forces

Higher Order Harmonic Balance Analysis for Limit Cycle Oscillations in an Airfoil with Cubic Restoring Forces

著者名:

Liu, L. ( University of Texas Pan American, Edinburg, TX )
Dowell, E. ( Duke University, Durham, NC )
Thomas, J.

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

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

シリーズ巻号:

46th

発行年:

2005

通号:

2005-1918

ペーパー番号:

AIAA Paper 2005-1918

出版情報:

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

ISSN:

10877215

言語:

英語

請求記号:

A07400/200506 [CD-ROM 2005 Disc 6]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001621
シリーズID:	PA00000154
会議名:	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
回次:	46th
会議開催地:	Austin, Texas
会議開催年:	2005.04.18-2005.04.21

類似資料:

1 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	7 テクニカルペーパー Higher Order Harmonic Balance Analysis of an Airfoil with a Hysteretic Non-Linearity N. Amuyedo, J. Cooper American Institute of Aeronautics and Astronautics
2 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	8 テクニカルペーパー "Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter and Limit Cycle Oscillations" Thomas,J., Dowell,E., Hall,K. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー 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 テクニカルペーパー An Investigation of the Sensitivity of F-16 Fighter Flutter Onset and Limit Cycle Oscillations to Uncertainties J. Thomas, E. Dowell, K. Hall, C. Denegri American Institute of Aeronautics and Astronautics
4 テクニカルペーパー 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 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
5 テクニカルペーパー A Parameter Study of Transonic Airfoil Flutter and Limit Cycle Oscillation Behavior Kholodar, D., Thomas, J., Dowell, E., Hall, K. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Frequency and Amplitude Prediction of Limit Cycle Oscillations of an Airfoil Containing Concentrated Structural Nonlinearities Wong,Y.-S., Liu,L., Lee,B. American Institute of Aeronautics and Astronautics
6 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	12 テクニカルペーパー Brake Squeal Analysis: A New Method for Predicting Limit Cycles Using the Constraint Harmonic Balance Method. Coudeyras, N., Nacivet, S., Sinou, J.-J. Society of Automotive Engineers

1

2

3

4

5

6

7

8

9

10

11

12