Test Results on the ARL 19 Supersonic Blade Cascade

[+] Author and Article Information
A. Fourmaux, R. Gaillard, G. Losfeld, G. Meauzé

Office National d’Etudes et de Recherches Aérospatiales, BP 72-92322 Châtillon Cedex, France

J. Turbomach 110(4), 450-455 (Oct 01, 1988) (6 pages) doi:10.1115/1.3262218 History: Received January 25, 1988; Online November 09, 2009


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.

Copyright © 1988 by ASME
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