Analytical, Computational, and Experimental Investigations of Equivalence Between Pitch and Plunge Motions for Airfoils at Low Reynolds Numbers

Analytical, Computational, and Experimental Investigations of Equivalence Between Pitch and Plunge Motions for Airfoils at Low Reynolds Numbers

著者名:

G. McGowan ( North Carolina State University, Raleigh, NC )
A. Gopalarathnam
J. Edwards
M. Ol ( Air Force Research Lab, Wright-Patterson AFB, OH )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

2009

発行年:

2009

通号:

2009-0535

ペーパー番号:

AIAA Paper 2009-0535

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200901

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00052180
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition
回次:	47th
会議開催地:	Orlando, Florida
会議開催年:	2009.01.05-2009.01.08
論文注記:	47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 5-8 January 2009, Orlando, Florida

類似資料:

1 テクニカルペーパー Computation vs. Experiment for High-Frequency Low-Reynolds Number Airfoil Pitch and Plunge G. McGowan, A. Gopalarathnam, M. Ol, J. Edwards, D. Fredberg American Institute of Aeronautics and Astronautics	7 テクニカルペーパー An Experimental Study of Flexible Membrane Airfoils at Low Reynolds Numbers M. Tamai, J. Murphy, H. Hu American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Experimental Investigation of Pitching and Plunging Airfoils at Reynolds Number between 1x10^4 and 6x10^4 Baik, Yeon Sik, Rausch, Jonathan M, Bernal, Luis P, Ol, Michael V American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Fluid Dynamics of Pitching and Plunging Airfoils of Reynolds Number between 1×10₄ and 6×10₄ C. Kang, Y. Baik, L. Bernal, M. OL, W. Shyy American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Analytical and Computational Study of Adaptive Circulation Control Airfoils McGowan, G., Gopalarathnam, A., Jones, G. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Modeling of pitching and plunging airfoils at Reynolds number between 1x10^4 and 6x10^4 Kang, Chang Kwon, Aono, Hikaru, Trizila, Pat, Baik, Yeon, Rausch, Jonathan M., Bernal, Luis, Ol, Michael V., Shyy, Wei American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Vortical Structures in High Frequency Pitch and Plunge at Low Reynolds Number M. Ol American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Effects of Unequal Pitch and Plunge Airfoil Motion Frequency on Aerodynamic Response C. Webb, H. Dong, M. Ol American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Comparative Study of Pitch-Plunge Airfoil Aerodynamics at Transitional Reynolds Number Y. Lian, M. Ol, W. Shyy American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Computational Study of Free Flight of Low Reynolds Number Pitching Airfoils and Wings D. Chandar, M. Damodaran American Institute of Aeronautics and Astronautics
6 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	12 テクニカルペーパー Investigation of Airfoil Boundary Layer and Wake Development at Low Reynolds Numbers Yarusevych, S., Sullivan, P., Kawall, J. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12