Low Noise Design Trends Derived from wind tunnel Testing on Advanced High-Lift Devices

Low Noise Design Trends Derived from wind tunnel Testing on Advanced High-Lift Devices

Author(s):

M. Fischer ( Airbus Deutschland GmbH, Bremen, Germany )
H. Friedel ( Aachen University of Technology, Aachen, Germany )
H. Holthusen ( German-Dutch Wind Tunnels, Emmeloord, The Netherlands )
B. Gölling ( Deutsche Aerospace Airbus, GmbH, Bremen, Germany )
R. Emunds

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/CEAS Aeroacoustics Conference

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-2562

Paper no.:

AIAA Paper 2006-2562

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200608 [CD-ROM 2006 Disc 8]

Type:

Technical Paper

Details

TDL ID:	ZA00047229
Series ID:	PA00000149
Conf. info. (Name):	AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference)
Conf. info. (Number):	12th
Conf. info. (Venue):	Cambridge, Massachusetts
Conf. info. (Date):	2006.05.08-2006.05.10

Similar Items:

1 Technical Paper CAA in Industrial Environment: First Analysis of Noise Sources on a 2D High-Lift Profile at Airbus Bieler, H., Fischer, M., Emunds, R., Sutcliffe, M. American Institute of Aeronautics and Astronautics	7 Technical Paper Design and testing of a low self-noise aerodynamic microphone forebody Dassen, Ton, Holthusen, Hermann, Beukema, Martijn American Institute of Aeronautics and Astronautics
2 Technical Paper Effect of Re-Number, Ma-Number and Angle of Attack on Slat Noise Based on a Test Vortex Injected Upstream of the SLAT-Hook Emunds, R., Fischer, M. American Institute of Aeronautics and Astronautics	8 Technical Paper WIND TUNNEL WALL INTERFERENCE IN VSTOL AND HIGH LIFT TESTING: A SELECTED, ANNOTATED BIBLIOGRAPHY Tuttle, M.H. National Aeronautics and Space Administration
3 Technical Paper Effect of Slat Settings (Gap Overlap) on Slat Noise based on a test vortex injected upstream of the SLAT-Hook R. Emunds, M. Fischer American Institute of Aeronautics and Astronautics	9 Technical Paper Source location by phased array measurements in closed wind tunnel test sections Sijtsma, Pieter, Holthusen, Hermann American Institute of Aeronautics and Astronautics
4 Technical Paper An Integrated Design Approach for Low Noise Exposing High-Lift Devices J. Wild, M. Pott-Pollenske, B. Nagel American Institute of Aeronautics and Astronautics	10 Technical Paper PIV Measurement of a High-Lift-Device Model in JAXA 6.5m ﾗ 5.5m Low-Speed Wind Tunnel H. Kato, S. Watanabe, T. Hashimoto, K. Fujii, T. Ito, K. Yamamoto American Institute of Aeronautics and Astronautics
5 Technical Paper Phased Array Measurement of High Lift Devices in Low Speed Wind Tunnel H. Ura, Y. Yokokawa, T. Ito American Institute of Aeronautics and Astronautics	11 Technical Paper Low-Speed Wind Tunnel Tests on a Lambda Wing High-Lift Configuration Ghee, T., Taylor, N. American Institute of Aeronautics and Astronautics
6 Technical Paper High-Lift Device Testing in JAXA 6.5M X 5.5M Low-Speed Wind Tunnel T. Ito, Y. Yokokawa, H. Ura, H. Kato, K. Mitsuo, K. Yamamoto American Institute of Aeronautics and Astronautics	12 Technical Paper Low-Speed Wind Tunnel Tests on a Diamond Wing High-Lift Configuration Ghee,T., Taylor,N. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12