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
Link To Document :
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