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An experimental investigation of straight and curved annular wall jetsAccurate turbulence measurements taken in wall jet flows are difficult to obtain, due to high intensity turbulence and problems in achieving two-dimensionality. The problem is compounded when streamwise curvature of the flow is introduced, since the jet entrainment and turbulence levels are greatly increased over the equivalent planar values. In this experiment, two-dimensional straight and curved incompressible wall jet flows are simulated by having a jet blow axially over a cylinder. Hot wire measurements and some Laser Doppler Velocimetry measurements are presented for straight and curved wall jet flows. The results for the straight wall showed good agreement between the annular flow data and the rectangular data taken by previous researchers. For the jets with streamwise curvature, there was agreement between the annular and corresponding rectangular jets for the flow region closest to the slot exit. An integral analysis was used as a simple technique to interpret the experimental results. Integral momentum calculations were performed for both straight and curved annular and two dimensional wall jets. The results of the calculation were used to identify transverse curvature parameters and to predict the values of those parameters which would delineate the region where the annular flow can satisfactorily simulate two dimensional flow.
Document ID
19880009173
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rodman, L. C.
(Stanford Univ. CA, United States)
Wood, N. J.
(Stanford Univ. CA, United States)
Roberts, L.
(Stanford Univ. CA, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:182546
NASA-CR-182546
JIAA-TR-79
Report Number: NAS 1.26:182546
Report Number: NASA-CR-182546
Report Number: JIAA-TR-79
Accession Number
88N18557
Funding Number(s)
CONTRACT_GRANT: NCC2-173
CONTRACT_GRANT: NCC2-376
CONTRACT_GRANT: NCC2-331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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