Numerical Analysis for Transonic Cascade Flows Using the AF2 Scheme

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概要

• 論文の詳細を見る

• An approximate factorization code has been developed for analyzing transonic cascade flows. In this scheme, upwind differencing is used for introducing artificial viscosity in the supersonic region, and central differencing in the subsonic region. The resulting simple two- and three-banded matrices are solved by the relaxation procedure. In this paper, the efficiency of this scheme is demonstrated by solving a channel flow problem, and then this scheme is applied to some cascade flows. The results are in good agreement with those obtained by other methods.

• 一般社団法人日本機械学会の論文

著者

• Tamaki Teiichi

  Ishikawajima Harima Heavy Industries Co. Ltd.

• SATOFUKA Nobuyuki

  Kyoto Institute of Technology

• NISHIDA Hidetoshi

  Kyoto Institute of Technology

• SHIMIZU Atsushi

  Ishikawajima-Harima Heavy Industries Co., Ltd.

• Shimizu Atsushi

  Ishikawajima-harima Heavy Industries Co. Ltd.

関連論文

• Report on Organized Sessions
• AIRCRAFT GAS TURBINES(Activities in the Field of Gas Turbines and Turbochargers in Japan)
• Organized Session V: Advanced Propulsion Technology for Subsonic Civil Transport(Report on Organized Sessions,1995 Yokohama International Gas Turbine Congress)
• Numerical Analysis for Transonic Cascade Flows Using the AF2 Scheme
• AIRCRAFT GAS TURBINES(Activities in the Field of Gas Turbines and Turbochargers in Japan)
• A Numerical Study of Shock Formation in Cylindrircal and Two-Dimensional Shock Tubes

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