Comparison of RANS Simulations of Multi-Element High-Lift Configurations

Comparison of RANS Simulations of Multi-Element High-Lift Configurations

Author(s):

M. Murayama ( Japan Aerospace Exploration Agency, Chofu, Japan )
T. Imamura
K. Yamamoto
K. Kobayashi ( Ryoyu Systems Company, Ltd., Minato-ku, Japan )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-1396

Paper no.:

AIAA Paper 2006-1396

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200602 [CD-ROM 2006 Disc 2]

Type:

Technical Paper

Details

TDL ID:	ZA00047217
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	44th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2006.01.09-2009.01.12

Similar Items:

1 Technical Paper Validation of Flows on High-Lift Configurations by Structured and Unstructured Mesh Method Murayama, M., Yamamoto, K., Kobayashi, K. American Institute of Aeronautics and Astronautics	7 Technical Paper Investigation of Airframe Noise from High Lift Configuration Model H. Ura, Y. Yokokawa, T. Imamura, T. Ito, K. Yamamoto American Institute of Aeronautics and Astronautics
2 Technical Paper Experiment and CFD of a High-Lift Configuration Civil Transport Aircraft Model Y. Yokokawa, M. Murayama, T. Ito, K. Yamamoto American Institute of Aeronautics and Astronautics	8 Technical Paper RANS Simulation Over JAXA High-Lift Configuration Model Using Spectral Volume Method T. Haga, M. Furudate, K. Sawada, A. Masunaga American Institute of Aeronautics and Astronautics
3 Technical Paper CFD Validation Study for a High-Lift Configuration of a Civil Aircraft Model M. Murayama, Y. Yokokawa, K. Yamamoto, Y. Ueda American Institute of Aeronautics and Astronautics	9 Technical Paper Simulation of the Broadband Noise from a Slat Using Zonal LES/RANS Hybrid Method T. Imamura, S. Enomoto, Y. Yokokawa, K. Yamamoto American Institute of Aeronautics and Astronautics
4 Technical Paper Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel M. Murayama, Y. Yokokawa, K. Tanaka, K. Yamamoto, T. Ito American Institute of Aeronautics and Astronautics	10 Technical Paper High-Lift Wing Design in Consideration of Sweep Angle Effect Using Kriging Model M. Kanazaki, T. Imamura, S. Jeong, K. Yamamoto American Institute of Aeronautics and Astronautics
5 Technical Paper A Far-field Noise and Near-field Unsteadiness of a Simplified High-lift-configuration Model (Slat) T. Imamura, H. Ura, Y. Yokokawa, K. Yamamoto American Institute of Aeronautics and Astronautics	11 Technical Paper Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing Y. Yokokawa, M. Murayama, M. Kanazaki, K. Murota, T. Ito, K. Yamamoto American Institute of Aeronautics and Astronautics
6 Technical Paper A Far-Field Noise and Near-Field Unsteadiness of a Simplified High-Lift-Configuration Model (Flap-Edge) Y. Yokokawa, T. Imamura, H. Ura, K. Yamamoto American Institute of Aeronautics and Astronautics	12 Technical Paper Numerical and Experimental Research of Low-Noise Slat Using Simplified High-lift Model T. Imamura, H. Ura,, Y. Yokokawa, T. Hirai, K. Yamamoto American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12