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Entrainment and thrust augmentation in pulsatile ejector flowsThis study comprised direct thrust measurements, flow visualization by use of a spark shadowgraph technique, and mean and fluctuating velocity measurements with a pitot tube and linearized constant temperature hot-wire anemometry respectively. A gain in thrust of as much as 10 to 15% was observed for the pulsatile ejector flow as compared to the steady flow configuration. From the velocity profile measurements, it is concluded that this enhanced augmentation for pulsatile flow as compared to a nonpulsatile one was accomplished by a corresponding increased entrainment by the primary jet flow. It is also concluded that the augmentation and total entrainment by a constant area ejector critically depends upon the inlet geometry of the ejector. Experiments were performed to evaluate the influence of primary jet to ejector area ratio, ejector length, and presence of a diffuser on pulsatile ejector performance.
Document ID
19810021591
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sarohia, V.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bernal, L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bui, T.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 4, 2013
Publication Date
August 15, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
JPL-PUB-81-36
NASA-CR-164715
Report Number: JPL-PUB-81-36
Report Number: NASA-CR-164715
Accession Number
81N30129
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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