Test Results on the ARL 19 Supersonic Blade Cascade
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This paper presents the ONERA contribution in a joint experimental program on the aerodynamics of supersonic airfoil cascades. The first part deals with the specific ONERA way of running cascade tests: description of the test facility, the test model, the instrumentation, and data reduction. Then, after a brief theoretical analysis of the ARL 19 cascade, some experimental results are presented and discussed.
1996 ◽
Vol 05
(04)
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pp. 653-670
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1983 ◽
Vol 105
(2)
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pp. 348-353
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2011 ◽
Vol 243-249
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pp. 1528-1535
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2011 ◽
Vol 261-263
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pp. 989-993
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2013 ◽
Vol 300-301
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pp. 382-388
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