Theory of Mutual Interference in Tandem Compressor Cascade

DOI DOI Web Site Web Site Web Site 1 Citations

Bibliographic Information

Other Title
  • 二重圧縮機翼列における相互干渉の理論
  • ニジュウ アッシュクキヨクレツ ニ オケル ソウゴ カンショウ ノ リロン

Search this article

Abstract

Two adjacent rows of blades, which constitute a tandem compressor cascade, interfere aerodynamically with each other, so that the deflection angle and losses are different from those of a system having no interference. In order to calculate the interference effect on cascade performance, a method must be found for calculating the change of flow field due to interference. This paper presents a theoretical method for determining the two-dimensional incompressible potential flow through an arbitrary tandem compressor cascade based on a singularity method. This theory is especially suitable for the case in which the relative position between the two blade rows varies, while the blade profiles and settings remain constant. Results of sample calculation are shown and compared with the corresponding experimental results.

Journal

Citations (1)*help

See more

Details 詳細情報について

Report a problem

Back to top