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Surge-Inception Study in a Two-Spool Turbojet Engine, Revised
"A two-spool turbojet engine was operated in the Lewis altitude wind tunnel to study the inception of compressor surge. In addition to the usual steady-state pressure and temperature measurements, the compressors were extensively instrumented with fast-response interstage pressure transducers. Thus it was possible to obtain maps for both compressors, pressure oscillations during rotating stall, effects of stall on efficiency, and stage-loading curves" (p. 1).
Date:
November 12, 1957
Creator:
Wallner, Lewis E.; Lubick, Robert J. & Saari, Martin J.
System:
The UNT Digital Library