Dynamic Stall Alleviation using a Deformable Leading Edge Concept - A Numerical Study | 東京工業大学附属図書館文献データベース

Dynamic Stall Alleviation using a Deformable Leading Edge Concept - A Numerical Study

Author(s):

Sahin, Mehmet ( School of Aerospace Engineering Georgia Institute of Technology )
Sankar, Lakshmi N.
Chandrasekhara, M. S.
Tung, Chee

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-0520

Paper no.:

00-0520

Page(from):

1

Page(to):

13

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050874
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospaces Science Meeting and Exhibit
Conf. info. (Number):	38th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2000.01.10-2000.01.13
Note for article:	38th Aerospace Sciences Meeting & Exhibit 10-13 January 2000 / Reno, NV

Similar Items:

1 Technical Paper Numerical Studies of Stall and Surge Alleviation in a High-Speed Transonic Fan Rotor Niazi, Saeid, Stein, Alex, Sankar, Lakshmi N. American Institute of Aeronautics and Astronautics	7 Technical Paper Computational Analysis of Stall Control Using Bleed Valve in a High-Speed Compressor Niazi, Saeid, Stein, Alexander, Sankar, Lakshmi. N. American Institute of Aeronautics and Astronautics
2 Technical Paper Compressible Dynamic Stall Performance of a Variable Droop Leading Edge Airfoil with a Gurney Flap Chandrasekhara, M., Martin, P., Tung, C. American Institute of Aeronautics and Astronautics	8 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
3 Technical Paper A Computational Investigation of Dynamic Stall Alleviation using Leading Edge Deformation Reuster,J., Baeder,J. American Institute of Aeronautics and Astronautics	9 Technical Paper Compressible dynamic stall control using a shape adaptive airfoil Chandrasekhara, M.S., Wilder, M.C., Carr, L.W. American Institute of Aeronautics and Astronautics
4 Technical Paper Heat Flux Gage Studies of Compressible Dynamic Stall. Chandrasekhara, M.S., Wilder, M.C. American Institute of Aeronautics and Astronautics	10 Technical Paper On the competing mechanisms of compressible dynamic stall Chandrasekhara, M.S., Wilder, M.C., Carr, L.W. American Institute of Aeronautics and Astronautics
5 Technical Paper Compressible Dynamic Stall Control Using a Shape Adaptive Airfoil Chandrasekhara, M. S., Wilder, M. C., Carr, L. W. American Institute of Aeronautics and Astronautics	11 Technical Paper Interferometric Investigations of Compressible Dynamic Stall Over a Transiently Pitching Airfoil Chandrasekhara, M.S., Carr, L.W. National Aeronautics and Space Adminstration
6 Technical Paper Suppression of Cavity Loads Using Leading Edge Blowing Concepts S. Arunajatesan, C. Kannepalli, N. Sinha, M. Sheehan, G. Shumway American Institute of Aeronautics and Astronautics	12 Technical Paper Reduction of BVI noise using a leading edge air mass injection concept ; a numerical study using large-eddy simulation Ilie, Marcel American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12