Publication Date:
2019-06-27
Description:
The design of the 3 1/2-stage turbine is described, and the cold-air performance of the first stage, modified for axial inlet conditions, is presented. The performance of the modified single-stage turbine and of two comtemporary high-stage-loading-factor turbines is compared with that estimated with a reference prediction method.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-TM-X-3289
,
E-8354
Format:
application/pdf
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