Experimental investigation of compressor cascade wakes

D. E. Hobbs, J. H. Wagner, John Francis Dannenhoffer, R. P. Dring

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Abstract

This report discusses a cascade wake experiment intended to improve wake modeling in an airfoil analysis. The experiment included extensive measurements of the near and far wakes, trailing edge boundary layers, and airfoil surface static pressures. The measured wake displacement surface and computed boundary layers were used in conjunction with a cascade potential flow solver to demonstrate the feasibility of modeling the viscous aspects of cascade flow.

Original languageEnglish (US)
Title of host publicationProceedings of the ASME Turbo Expo
PublisherAmerican Society of Mechanical Engineers (ASME)
Volume1
ISBN (Print)9780791879566
DOIs
StatePublished - 1982
Externally publishedYes
EventASME 1982 International Gas Turbine Conference and Exhibit, GT 1982 - London, United Kingdom
Duration: Apr 18 1982Apr 22 1982

Other

OtherASME 1982 International Gas Turbine Conference and Exhibit, GT 1982
CountryUnited Kingdom
CityLondon
Period4/18/824/22/82

    Fingerprint

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Hobbs, D. E., Wagner, J. H., Dannenhoffer, J. F., & Dring, R. P. (1982). Experimental investigation of compressor cascade wakes. In Proceedings of the ASME Turbo Expo (Vol. 1). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/82-GT-299