Blank Cover Image

Motion Kinematics vs. Angle of Attack Effects in High-Frequency Airfoil Pitch/Plunge

著者名:
  • M. Ol ( U.S. Air Force Research Lab, Wright-Patterson AFB, OH )
  • H. Dong ( Wright State University, Dayton, OH )
  • C. Webb
掲載資料名:
AIAA meeting papers on disc
シリーズ名:
AIAA Paper : AIAA Fluid Dynamics Conference
シリーズ巻号:
2008
発行年:
2008
通号:
2008-3822
ペーパー番号:
AIAA Paper 2008-3822
出版情報:
Reston, Va.: American Institute of Aeronautics and Astronautics
ISSN:
10877215
言語:
英語
請求記号:
A07400/200807 [CD-ROM 2008 Disc 7]
資料種別:
テクニカルペーパー

類似資料:

1 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
7 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
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 Optimization of Unstalled Pitching and Plunging Motion of an Airfoil

S. Yang, S. Luo, F. Liu, H. Tsai

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 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
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 Robust Roll-Pitch-Yaw Integrated Autopilot for a High Angle-of-Attack Missile

S. Kang, H. Kim, D. Won, M-J. Tahk, J-I. Lee, B-E. Jun

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 Angle of Attack and Planform Effects on Flat Plate Vortices at Low Reynolds Numbers

S. Kaplan, A. Altman, M. Ol

American Institute of Aeronautics and Astronautics
6 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
12 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
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12