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Experimental design studies and flow visualization of proportional laminar-flow fluidic amplifiersThe effects of certain parameter variations on the performance characteristics of laminar, proportional, jet-deflection fluidic amplifiers were studied. The matching and staging of amplifiers to obtain high pressure gain was included, but dynamic effects were not. The parameter variations considered were aspect ratio, setback, control length, splitter distance, receiver-duct width, width of center-vent duct, and bias pressure. Usable pressure gains of 19 per stage were achieved, and 5 amplifier stages were integrated to yield an overall pressure gain of 2,000,000.
Document ID
19770026498
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hellbaum, R. F.
(NASA Langley Research Center Hampton, VA, United States)
Mcdermon, J. N.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1977
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
L-10868
NASA-TN-D-8433
Report Number: L-10868
Report Number: NASA-TN-D-8433
Accession Number
77N33442
Funding Number(s)
PROJECT: RTOP 512-52-02-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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