作者: S. O'Byrne , P.M. Danehy , A.F.P. Houwing
DOI: 10.1109/ICIASF.2003.1274863
关键词: Mechanics 、 Hypersonic speed 、 Flow velocity 、 Classical mechanics 、 Laminar flow 、 Displacement (vector) 、 Similarity solution 、 Vibrational energy relaxation 、 Physics 、 Rotational temperature 、 Boundary layer
摘要: 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 finite-volume computation first-order layer computation, assuming local similarity. Both computations produced similar nearly identical distributions. disagreement between calculations is ascribed the similarity solution not accounting for leading-edge displacement effects. agreed within measurement uncertainty of 2% with both calculated peak was 200 K lower than computed values. This discrepancy tentatively vibrational relaxation in layer.