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Fluid mechanics experiments in oscillatory flow. Volume 2: Tabulated dataResults of a fluid mechanics measurement program in oscillating flow within a circular duct are presented. The program began with a survey of transition behavior over a range of oscillation frequency and magnitude and continued with a detailed study at a single operating point. Such measurements were made in support of Stirling engine development. Values of three dimensionless parameters, Re sub max, Re sub w, and A sub R, embody the velocity amplitude, frequency of oscillation, and mean fluid displacement of the cycle, respectively. Measurements were first made over a range of these parameters that are representative of the heat exchanger tubes in the heater section of NASA's Stirling cycle Space Power Research Engine (SPRE). Measurements were taken of the axial and radial components of ensemble-averaged velocity and rms velocity fluctuation and the dominant Reynolds shear stress, at various radial positions for each of four axial stations. In each run, transition from laminar to turbulent flow, and its reverse, were identified and sufficient data was gathered to propose the transition mechanism. Volume 2 contains data reduction program listings and tabulated data (including its graphics).
Document ID
19920011949
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Seume, J.
(Minnesota Univ. Minneapolis, MN, United States)
Friedman, G.
(Minnesota Univ. Minneapolis, MN, United States)
Simon, T. W.
(Minnesota Univ. Minneapolis, MN, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-189128
NAS 1.26:189128
Report Number: NASA-CR-189128
Report Number: NAS 1.26:189128
Accession Number
92N21192
Funding Number(s)
PROJECT: RTOP 590-13-11
CONTRACT_GRANT: NAG3-598
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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