作者: J.M.M. Sousa , L.M.G. Silva
DOI: 10.1016/J.COMPSTRUC.2004.03.051
关键词:
摘要: Abstract The coupling of Navier–Stokes computations with e N method for transition prediction in infinite swept wings is demonstrated. In the present paper, results are presented illustrating successful these methods a 45° wing operating at four different Reynolds numbers. Moreover, main issues involved generation adapted meshes and computation mean flow by documented. all studied cases, subsequent linear stability analysis has shown that process was dominated cross-flow instability. have been validated against experimental data from literature.