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Preliminary design of an intermittent smoke flow visualization systemA prototype intermittent flow visualization system that was designed to study vortex flow field dynamics has been constructed and tested through its ground test phase. It produces discrete pulses of dense white smoke consisting of particles of terephthalic acid by the pulsing action of a fast-acting three-way valve. The trajectories of the smoke pulses can be tracked by a video imaging system without intruding in the flow around in flight. Two methods of pulsing the smoke were examined. The simplest and safest approach is to simply divert the smoke between the two outlet ports on the valve; this approach should be particularly effective if it were desired to inject smoke at two locations during the same test event. The second approach involves closing off one of the outlet ports to momentarily block the flow. The second approach requires careful control of valve dwell times to avoid excessive pressure buildup within the cartridge container. This method also increases the velocity of the smoke injected into the flow. The flow of the smoke has been blocked for periods ranging from 30 to 80 milliseconds, depending on the system volume and the length of time the valve is allowed to remain open between valve closings.
Document ID
19930019504
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ward, Donald T.
(Texas A&M Univ. College Station, TX, United States)
Myatt, James H.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1993
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-1917
NAS 1.26:186027
TEES-AERO-TR-91-1
NASA-CR-186027
Accession Number
93N28693
Funding Number(s)
PROJECT: RTOP 533-02-35
CONTRACT_GRANT: NAG2-651
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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