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INVESTIGATION OF A 0.6 HUB-TIP RADIUS-RATIO TRANSONIC TURBINE DESIGNED FOR SECONDARY-FLOW STUDY. III - EXPERIMENTAL PERFORMANCE WITH TWO STATOR CONFIGURATIONS DESIGNED TO ELIMINATE BLADE WAKES AND SECONDARY-FLOW EFFECTS AND CONCLUSIONS FROM ENTIRE STATOR INVESTIGATION
Moffitt, T. P., Rohlik, H. E., Wintucky, W. T.

INVESTIGATION OF A 0.6 HUB-TIP RADIUS-RATIO TRANSONIC TURBINE DESIGNED FOR SECONDARY-FLOW STUDY. III - EXPERIMENTAL PERFORMANCE WITH TWO STATOR CONFIGURATIONS DESIGNED TO ELIMINATE BLADE WAKES AND SECONDARY-FLOW EFFECTS AND CONCLUSIONS FROM ENTIRE STATOR INVESTIGATION

Aerospace & Aviation Published 2019 Verification Pending

Overview & Synopsis

Hub-tip radius ratio transonic turbine for secondary flow - stator configurations designed to eliminate blade wakes and secondary-flow effects

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Document Title INVESTIGATION OF A 0.6 HUB-TIP RADIUS-RATIO TRANSONIC TURBINE DESIGNED FOR SECONDARY-FLOW STUDY. III - EXPERIMENTAL PERFORMANCE WITH TWO STATOR CONFIGURATIONS DESIGNED TO ELIMINATE BLADE WAKES AND SECONDARY-FLOW EFFECTS AND CONCLUSIONS FROM ENTIRE STATOR INVESTIGATION
Author / Organization Moffitt, T. P., Rohlik, H. E., Wintucky, W. T.
Subject & Discipline OTHER
Categories Aerospace & Aviation
Publication Year 2019
License / Rights Public Domain / NASA STI Open Access
Resource Verification Listed PDF (Verification Pending)
Original Host Website NASA Technical Reports Server (ntrs.nasa.gov)
File Format application/pdf (Portable Document Format)
Language EN
Catalog ID DOC-69372
Original Source Link Visit Source Page on ntrs.nasa.gov »