Computation of unsteady 3-D transonic flow through gas turbuine cascade channel

Satoru Yamamoto, Takashi Shiraishi

Research output: Contribution to journalArticlepeer-review

1 Citation (Scopus)


Unsteady three-dimensional transonic viscous flows through a gas turbine cascade channel are numerically investigated using the higher-resolution shock-vortex capturing method proposed by the authors. The higher-resolution both in space discretization and time integration enables us to obtain real flow characteristics in the 3-D gas turbine cascade. As numerical results, calculated unsteady 3-D vortical structures in the wake and at the corner are shown, and obtained unsteady flow patterns near the blade under on-and off-design conditions are compared with eath other.

Original languageEnglish
Pages (from-to)2424-2430
Number of pages7
JournalNihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Issue number624
Publication statusPublished - 1998


  • CFD
  • FDM
  • Transonic flow
  • Turbomachinery
  • Unsteady flow


Dive into the research topics of 'Computation of unsteady 3-D transonic flow through gas turbuine cascade channel'. Together they form a unique fingerprint.

Cite this