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Experimental and analytical dynamic flow characteristics of an axial-flow fan from an air cushion landing system modelAn investigation was conducted to compare the steady-state and dynamic flow characteristics of an axial-flow fan which had been used previously as the air supply fan for some model air cushion landing system studies. Steady-state flow characteristics were determined in the standard manner by using differential orifice pressures for the flow regime from free flow to zero flow. In this same regime, a correlative technique was established so that fan inlet and outlet pressures could be used to measure dynamic flow as created by a rotating damper. Dynamic tests at damper frequencies up to 5 Hz showed very different flow characteristics when compared with steady-state flow, particularly with respect to peak pressures and the pressure-flow relationship at fan stall and unstall. A generalized, rational mathematical fan model was developed based on physical fan parameters and a steady-state flow characteristic. The model showed good correlation with experimental tests at damper frequencies up to 5 Hz.
Document ID
19770022228
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Thompson, W. C.
(NASA Langley Research Center Hampton, VA, United States)
Boghani, A. B.
(Foster-Miller Assoc., Inc. Hampton, VA, United States)
Leland, T. J. W.
(NASA Langley Research Center)
Date Acquired
September 3, 2013
Publication Date
July 1, 1977
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
L-11154
NASA-TN-D-8413
Report Number: L-11154
Report Number: NASA-TN-D-8413
Accession Number
77N29172
Funding Number(s)
PROJECT: RTOP 505-08-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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