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Large amplitude forcing of a high speed 2-dimensional jetThe effect of large amplitude forcing on the growth of a high speed two dimensional jet was investigated experimentally. Two forcing techniques were utilized: mass flow oscillations and a mechanical system. The mass flow oscillation tests were conducted at Strouhal numbers from 0.00052 to 0.045, and peak to peak amplitudes up to 50 percent of the mean exit velocity. The exit Mach number was varied in the range 0.15 to 0.8. The corresponding Reynolds numbers were 8,400 and 45,000. The results indicate no significant change of the jet growth rate or centerline velocity decay compared to the undisturbed free jet. The mechanical forcing system consists of two counter rotating hexagonal cylinders located parallel to the span of the nozzle. Forcing frequencies up to 1,500 Hz were tested. Both symmetric and antisymmetric forcing can be implemented. The results for antisymmetric forcing showed a significant (75 percent) increase of the jet growth rate at an exit Mach number of 0.25 and a Strouhal number of 0.019. At higher rotational speeds, the jet deflected laterally. A deflection angle of 39 deg with respect to the centerline was measured at the maximum rotational speed.
Document ID
19850014082
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bernal, L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sarohia, V.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 5, 2013
Publication Date
December 15, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
JPL-PUB-84-91
NAS 1.26:175646
NASA-CR-175646
Report Number: JPL-PUB-84-91
Report Number: NAS 1.26:175646
Report Number: NASA-CR-175646
Accession Number
85N22393
Funding Number(s)
CONTRACT_GRANT: NAS7-918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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