NASA Logo

NTRS

NTRS - NASA Technical Reports Server

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Flap Edge Noise Reduction FinsA flap of the type that is movably connected to an aircraft wing to provide control of an aircraft in flight includes opposite ends, wherein at least a first opposite end includes a plurality of substantially rigid, laterally extending protrusions that are spaced apart to form a plurality of fluidly interconnected passageways. The passageways have openings adjacent to upper and lower sides of the flap, and the passageways include a plurality of bends such that high pressure fluid flows from a high pressure region to a low pressure region to provide a boundary condition that inhibits noise resulting from airflow around the end of the flap.
Document ID
20150018775
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Khorrami, Mehdi R.
Choudhan, Meelan M.
Date Acquired
October 5, 2015
Publication Date
September 15, 2015
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-13/838,163
Patent Number: US-Patent-9,132,909
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,132,909
Patent Application
US-Patent-Appl-SN-13/838,163
No Preview Available