SAE Technical Paper Series 2011
DOI: 10.4271/2011-01-1617
|View full text |Cite
|
Sign up to set email alerts
|

Design of a Quiet Inlet for a 6×6 Boundary Layer Flow Duct

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2011
2011
2014
2014

Publication Types

Select...
2
2

Relationship

0
4

Authors

Journals

citations
Cited by 4 publications
(2 citation statements)
references
References 4 publications
0
2
0
Order By: Relevance
“…At the full 150 mm × 150 mm cross section, the tunnel can currently run up to Mach 0.6. Additional details on the flow facility, including acoustic characterization data, can be found in [35] and [36].…”
Section: Wind Tunnel Testingmentioning
confidence: 99%
“…At the full 150 mm × 150 mm cross section, the tunnel can currently run up to Mach 0.6. Additional details on the flow facility, including acoustic characterization data, can be found in [35] and [36].…”
Section: Wind Tunnel Testingmentioning
confidence: 99%
“…The flow duct has been described in detail elsewhere, including acoustic and turbulence measurements using pitot probes, hot wire anemometers, and kulite high intensity microphones [14,15]. The duct has been acoustically treated to reduce the facility acoustic noise as much as possible, including careful design of the mixer, diffuser, and nozzle, although measurements show that acoustic noise still dominates turbulent pressures at the wall for frequencies below approximately 400 Hz [15]. The system also includes a settling chamber and screens for straightening the flow and reducing turbulent intensity in the flow that enters the test section.…”
Section: Flow Duct Testingmentioning
confidence: 99%