IGTC-4 3-D Euler Solution Within Transonic Compressor and Trubine Blade(Session A-2 ANALYSIS OF CASCADE FLOW)

スポンサーリンク

概要

• 論文の詳細を見る

• A 3-D finite volume Euler code for flow field calculation within transonic compressor and turbine rotor or stator is presented in the paper. Four step Runge-Kutta scheme is chosen as a basic frame. The simple multi-grid approach is applied to accelerate the calculation. Absolute flow variables are solved in a Cartesian reference frame which may be rotating with an uniform angular velocity around x axis. Boundary conditions are described. One transonic turbine stator and one transonic compressore rotor are taken as numerical examples and the results are compared with experimental data and with that from other code. Very good agreement is found both for turbine stator blade and for compressor rotor.

• 公益社団法人日本ガスタービン学会の論文

著者

• Zhang Zhi-fang

  Shenyang Aero-engine Research Institute

• Wang L.C.

  Nanjing Aeronautial Institute

• Shi Z.H.

  Nanjing Aeronautial Institute

関連論文

• IGTC-4 3-D Euler Solution Within Transonic Compressor and Trubine Blade(Session A-2 ANALYSIS OF CASCADE FLOW)

スポンサーリンク