Phase-Resolved Surface Pressure and Heat-Transfer Measurements on the Blade of a Two-Stage Turbine

[+] Author and Article Information
M. G. Dunn, C. W. Haldeman

Calspan-UB Research Center, Buffalo, NY 14225

J. Fluids Eng 117(4), 653-658 (Dec 01, 1995) (6 pages) doi:10.1115/1.2817318 History: Received April 20, 1994; Revised May 31, 1995; Online December 04, 2007


Phase-resolved surface pressure, and unsteady pressure measurements are reported for the first-stage blade row of the Space Shuttle Main Engine two-stage fuel-side turbine. Measurements were made at 10, 50, and 90 percent span on both the pressure and suction surfaces of the blade. Phase-resolved and unsteady heat-flux measurements are also reported.

Copyright © 1995 by The American Society of Mechanical Engineers
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