6th Aeroacoustics Conference and Exhibit 2000
DOI: 10.2514/6.2000-1975
|View full text |Cite
|
Sign up to set email alerts
|

Flap edge aeroacoustic measurements and predictions

Abstract: ABSTRACTwhich was constructed to electronically steer to different regions of the model and to obtain farfield noise spectra and directivity from these regions.

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2009
2009
2019
2019

Publication Types

Select...
4
1

Relationship

0
5

Authors

Journals

citations
Cited by 20 publications
(1 citation statement)
references
References 16 publications
0
1
0
Order By: Relevance
“…Additional studies about the noise-generation mechanisms for trailing-edge noise, flaps, slats, and landing gears involving microphone arrays were performed at the Quiet Flow Facility in NASA Langley [94,[195][196][197][198][199]…”
Section: Open-jet Wind Tunnelsmentioning
confidence: 99%
“…Additional studies about the noise-generation mechanisms for trailing-edge noise, flaps, slats, and landing gears involving microphone arrays were performed at the Quiet Flow Facility in NASA Langley [94,[195][196][197][198][199]…”
Section: Open-jet Wind Tunnelsmentioning
confidence: 99%