Publication Date:
2019-06-27
Description:
The results of the high lift blade configuration design study are reported. The three-stage constant-inside-diameter turbine utilizes a ten degree tangentially leaned stator in stage three. All other bladerows use plain blades. Analysis of the leaned stator is discussed, and detailed design data are summarized. Steady-state stresses are discussed, and the results of the mechanical design analysis are presented.
Keywords:
PROPULSION SYSTEMS
Type:
NASA-CR-2096
,
R71AEG309
Format:
application/pdf
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