Effects of Unequal Pitch and Plunge Airfoil Motion Frequency on Aerodynamic Response

Effects of Unequal Pitch and Plunge Airfoil Motion Frequency on Aerodynamic Response

著者名:

C. Webb ( Wright State University, Dayton, OH )
H. Dong
M. Ol ( Air Force Research Laboratory/Wright-Patterson AFB, Dayton, 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:

2008

発行年:

2008

通号:

2008-0582

ペーパー番号:

AIAA Paper 2008-0582

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200801 [CD-ROM 2008 Disc 1]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00049519
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	46th
会議開催地:	Reno, Nevada
会議開催年:	2008.01.07-2008.01.10
論文注記:	46th AIAA Aerospace Sciences Meeting and Exhibit, 7-10 January 2008, Reno, Nevada

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1 テクニカルペーパー Motion Kinematics vs. Angle of Attack Effects in High-Frequency Airfoil Pitch/Plunge M. Ol, H. Dong, C. Webb American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Optimization of Unstalled Pitching and Plunging Motion of an Airfoil S. Yang, S. Luo, F. Liu, H. Tsai American Institute of Aeronautics and Astronautics
2 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	8 テクニカルペーパー Analytical, Computational, and Experimental Investigations of Equivalence Between Pitch and Plunge Motions for Airfoils at Low Reynolds Numbers G. McGowan, A. Gopalarathnam, J. Edwards, M. Ol American Institute of Aeronautics and Astronautics
3 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	9 テクニカルペーパー Unsteady force measurements in pitching-plunging airfoils Bernal, Luis P., Ol, Michael V., Szczublewski, Douglas P., Cox, Craig A. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Motion Kinematics Effects on Aerodynamic Performance of Bio-Inspired Wing Sections in Ultra-Low Reynolds Number Flow C. Webb, H. Dong, R. Mittal American Institute of Aeronautics and Astronautics	10 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
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 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
6 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	12 テクニカルペーパー The high-frequency, high-amplitude pitch problem: Airfoils, plates and wings Ol, Michael V. American Institute of Aeronautics and Astronautics

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