CALCULATION OF TWO- AND THREE-DIMENSIONAL TRANSONIC CASCADE FLOW FIELD USING THE NAVIER-STOKES EQUATIONS.

B. C. Weinberg, R. J. Yang, S. J. Shamroth, H. McDonald

研究成果: Conference article同行評審

摘要

Major objectives of the HOST program have been to improve hot section performance and life. Of specific interest here is the turbine, and in order to achieve the HOST objectives, accurate determinations of turbine blade pressure distributions and associated heat transfer rates are required. This paper applies a Navier-Stokes analysis employing the time-dependent Linearized Block Implicit scheme (LBI) of Briley and McDonald to two-dimensional and three-dimensional transonic turbulent cascade flows. In general, the geometrical configuration of the turbine blade impacts both the grid construction procedure and the implementation of the numerical algorithm.

原文English
頁(從 - 到)365-372
頁數8
期刊NASA Conference Publication
出版狀態Published - 1984 十二月 1

All Science Journal Classification (ASJC) codes

  • 航空工程

指紋

深入研究「CALCULATION OF TWO- AND THREE-DIMENSIONAL TRANSONIC CASCADE FLOW FIELD USING THE NAVIER-STOKES EQUATIONS.」主題。共同形成了獨特的指紋。

引用此