Prediction of a Thin-Airfoil Stall Phenomenon Using LES/RANS Hybrid Methodology with Compact Difference Scheme

Prediction of a Thin-Airfoil Stall Phenomenon Using LES/RANS Hybrid Methodology with Compact Difference Scheme

Author(s):

Kawai, S. ( University of Tokyo, Sagamihara, Japan )
Fujii, K. ( Institute of Space and Astronautical Science, Kanagawa, Japan )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Fluid Dynamics Conference

Ser. no.:

34th

Pub. Year:

2004

No.:

2004-2714

Paper no.:

AIAA-2004-2714

Pub. info.:

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

ISSN:

10877215

Language:

English

Call no.:

A07400/200410 [CD-ROM 2004 Disc 10]

Type:

Technical Paper

Details

TDL ID:	ZA00001607
Series ID:	PA00000147
Conf. info. (Name):	AIAA Fluid Dynamics Conference and Exhibit
Conf. info. (Number):	34th
Conf. info. (Venue):	Portland, Oregon
Conf. info. (Date):	2004.06.28-2004.07.01

Similar Items:

1 Technical Paper Computational Study of a Supersonic Base Flow Using LES/RANS Hybrid Methodology Kawai,S., Fujii,K. American Institute of Aeronautics and Astronautics	7 Technical Paper Large-Eddy Simulation of Compressible Transitional Boundary Layer S. Kawai, K. Fujii American Institute of Aeronautics and Astronautics
2 Technical Paper Compact Differencing and Filtering Schemes for Large-Eddy Simulation of Compressible Transitional Boundary Layer S. Kawai, K. Fujii American Institute of Aeronautics and Astronautics	8 Technical Paper Computatinal Analysis of the Characteristics of Subsonic, Transonic and Supersonic Base Flows Kawai, S., Fujii, K. American Institute of Aeronautics and Astronautics
3 Technical Paper LES of Compressible Turbulent Flows: Assessment of Compact Differencing with Localized Artificial Diffusivity Scheme S. Kawai, S. Shankar, S. Lele American Institute of Aeronautics and Astronautics	9 Technical Paper The effect of compressibility on suppression of dynamic stall using a slotted airfoil Carr, L.W., Chandrasekhara, M.S., Wilder, M.C., Noonan, K.W. American Institute of Aeronautics and Astronautics
4 Technical Paper Application of High-Order Compact Difference Scheme to Vortical Flow Computation over a Delta and Double-Delta Wings Arasawa, T., Fujii, K., Miyaji, K. American Institute of Aeronautics and Astronautics	10 Technical Paper Prediction of Sound Generated by a Pitching Airfoil: A Comparison of RANS and LES S. Nagarajan, S. Hahn, S. Lele American Institute of Aeronautics and Astronautics
5 Technical Paper Modeling Swirling Jet Flows Using a Hybrid RANS/LES Methodology J. Chenoweth, C. Kannepalli, S. Arunajatesan, A. Hosangadi American Institute of Aeronautics and Astronautics	11 Technical Paper ON THE USE OF COMPACT SCHEMES WITH SPATIAL FILTERING IN COMPUTATIONAL AEROACOUSTICS Koutsavdis, E. K., Blaisdell, G. A., Lyrintzis, A. S. American Institute of Aeronautics and Astronautics
6 Technical Paper Time-Series and Time-Averaged Characteristics of Subsonic to Supersonic Base Flows S. Kawai, K. Fujii American Institute of Aeronautics and Astronautics	12 Technical Paper Numerical Study of Flow Past a Circular Cylinder Using RANS, Hybrid RANS /LES and PANS Formulations Elmiligui, A., Abdol-Hamid, K., Massey, S., Pao, S. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12