Study of flow-field interactions in a transonic compressor using DPIV

Author:

Estevadeordal J.1,Gogineni S.1,Goss L.1,Copenhaver W.2,Gorrell S.2

Affiliation:

1. Innovative Scientific Solutions, Inc., Dayton, OH

2. USAF, Research Lab., Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. z Global Local Seeding Seeding Fig. 1 Flow pathofthe2000-hpCompressorAerodynamicResearchLaboratoryfacility (CARL).

2. Fig. 8 Flow visualization for half period of the blade passagein front of the WG at 20 psec intervals for the 24 WG configuration at 75% span (a, c) and 90 % span (b, d) for Close-spacing (a, b) and Mid-spacing (c, d). Scale is 1:l except for b (2:l). Percentages at the top and bottom of the last frames of each set indicate the span of the laser sheet. Letter à'above vortices denotestheir downstream convection. e (c)2000 American Institute of Aeronautics & Astronautics or published with permission of author(s) and/or author(s)' sponsoring organization.'

3. Vel (m/s): 0 20 40 60 80 100 128 140 160 l802Wl220240 260 280 300

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