Progress with 3D inverse method for turbomachine blade design

T. Dang, S. Damle, X. Qiu

Research output: Contribution to conferencePaper

Abstract

Improvements of turbomachine blade aerodynamic performance require proper tailoring of the three-dimensional blade profile. At the present time, techniques employed to arrive at the initial shapes of the blade geometry are at most quasi-3D methods. These methods cannot model the highly complex three-dimensional flowfield in the endwall regions (secondary flows and clearance effects) and multistage effects (streamwise vorticity and unsteady wakes). In this paper, we summarize our progress in the development of a fully 3D and viscous inverse method to upgrade the blade generation module used in existing blade design systems. This new 'blade-geometry generation' module will help turbomachine designers to design high-efficiency blades and shorten the blade design cycle. The work described here is critical to the development of high-efficiency turbomachine components for advanced utility and industrial gas turbines.

Original languageEnglish (US)
Pages7
Number of pages1
StatePublished - Dec 1 1998
EventProceedings of the 1998 ASME Energy Sources Technology Conference - Houston, TX, USA
Duration: Feb 2 1998Feb 4 1998

Other

OtherProceedings of the 1998 ASME Energy Sources Technology Conference
CityHouston, TX, USA
Period2/2/982/4/98

ASJC Scopus subject areas

  • Geology
  • Geotechnical Engineering and Engineering Geology

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    Dang, T., Damle, S., & Qiu, X. (1998). Progress with 3D inverse method for turbomachine blade design. 7. Paper presented at Proceedings of the 1998 ASME Energy Sources Technology Conference, Houston, TX, USA, .