Design of aspirated compressor blades using three-dimensional inverse method

T. Q. Dang, M. P.C. Van Rooij, L. M. Larosiliere

Research output: Contribution to conferencePaperpeer-review

14 Scopus citations

Abstract

A three-dimensional viscous inverse method is extended to allow blading design with full interaction between the prescribed pressure-loading distribution and a specified transpiration scheme. Transpiration on blade surfaces and endwalls is implemented as inflow/outflow boundary conditions, and the basic modifications to the method are outlined. This paper focuses on a discussion concerning an application of the method to the design and analysis of a supersonic rotor with aspiration. Results show that an optimum combination of pressure-loading tailoring with surface aspiration can lead to a minimization of the amount of sucked flow required for a net performance improvement at design and off-design operations.

Original languageEnglish (US)
Pages479-488
Number of pages10
DOIs
StatePublished - 2003
Event2003 ASME Turbo Expo - Atlanta, GA, United States
Duration: Jun 16 2003Jun 19 2003

Other

Other2003 ASME Turbo Expo
Country/TerritoryUnited States
CityAtlanta, GA
Period6/16/036/19/03

Keywords

  • Aspirated blades
  • Compressor aerodynamics
  • Inverse design

ASJC Scopus subject areas

  • Engineering(all)

Fingerprint

Dive into the research topics of 'Design of aspirated compressor blades using three-dimensional inverse method'. Together they form a unique fingerprint.

Cite this