DocumentCode
2655464
Title
Plif temperature and velocity distributions in laminar hypersonic flat-plate flow
Author
O´Byrne, S. ; Danehy, P.M. ; Houwing, A.F.P.
Author_Institution
NASA Langley Res. Center, Hampton, VA, USA
fYear
2003
fDate
25-29 Aug. 2003
Firstpage
136
Lastpage
147
Abstract
Rotational temperature and velocity distributions have been measured across a hypersonic laminar flat-plate boundary layer, using planar laser-induced fluorescence. The measurements are compared to a finite-volume computation and a first-order boundary layer computation, assuming local similarity. Both computations produced similar temperature distributions and nearly identical velocity distributions. The disagreement between calculations is ascribed to the similarity solution not accounting for leading-edge displacement effects. The velocity measurements agreed to within the measurement uncertainty of 2% with both calculated distributions. The peak measured temperature was 200 K lower than the computed values. This discrepancy is tentatively ascribed to vibrational relaxation in the boundary layer.
Keywords
boundary layers; computational fluid dynamics; finite volume methods; flow measurement; hypersonic flow; laminar flow; temperature distribution; velocity measurement; 200 K; edge displacement effects; finite volume computation; first order boundary layer computation; hypersonic flat plate flow; hypersonic laminar flat plate boundary layer; laminar flow; planar laser induced fluorescence; plif temperature distribution; rotational temperature; velocity distributions; velocity measurement; vibrational relaxation; Australia; Distributed computing; Electric shock; Fluid flow measurement; Fluorescence; Measurement uncertainty; Performance evaluation; Temperature distribution; Testing; Velocity measurement;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on
Print_ISBN
0-7803-8149-1
Type
conf
DOI
10.1109/ICIASF.2003.1274863
Filename
1274863
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