Leading Edge Deformation for Dynamic Stall Control

Leading Edge Deformation for Dynamic Stall Control

著者名:

Reuster,J.G. ( University of Maryland )
Baeder,J.D.

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

2001

発行年:

2001

通号:

2001-0120

ペーパー番号:

AIAA-2001-0120

開始ページ:

1

終了ページ:

11

総ページ数:

11

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050880
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting & Exhibit
回次:	39th
会議開催地:	Reno, Nevada
会議開催年:	2001.01.08-2001.01.11
論文注記:	39th AIAA Aerospace Sciences Meeting & Exhibit January 8-11, 2001/Reno, NV

類似資料:

1 テクニカルペーパー A Computational Investigation of Dynamic Stall Alleviation using Leading Edge Deformation Reuster,J., Baeder,J. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Computational Investigation of Trailing Edge Flap for Control of Vibration A. Mishra, J. Sitaraman, J. Baeder, D. Opoku American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Dynamic Stall From Pitching and Plunging Airfoil Motions. Reuster, J.G. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Active Flow Control Concepts for Rotor Airfoils Using Synthetic Jets. Duraisamy, K., Baeder, J.D. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Effects of Plunging on Flow Control for Pitching Airfoils Reuster,J.G. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Effect on Dynamic Stall on Cambered Airfoil with Drooping Leading Edge Control H. Qureshi, H. Hamdani, K. Parvez American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Effect of Leading-Edge Curvature and Slot Geometry on Dynamic Stall Control. Greenblatt, D., Wygnanski, I. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Stall Margin Improvement Using Feedback Control to Mitigate Inlet Distortion Unsteadiness. Warfield, Z., Paduano, J.D., MacMartin, D.G. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Coupled CFD/CSD Prediction of the Effects of Trailing Edge Flaps on Rotorcraft Dynamic Stall Alleviation A. Mishra, S. Ananthan, J. Baeder American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Euler Solutions to Nonlinear Acoustics of Non-Lifting Hovering Rotor Blades Baeder, J.D. National Aeronautics and Space Adminstration
6 テクニカルペーパー Unsteady Transition Phenomena at a Compressor Blade Leading Edge. Henderson, A.D., Walker, G.J., Hughes, J.D. American Society of Mechanical Engineers	12 テクニカルペーパー Observations of Transition Phenomena on a Controlled Diffusion Compressor Stator with a Circular Arc Leading Edge. Henderson, A.D., Walker, G.J. American Society of Mechanical Engineers

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