NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
INVESTIGATION OF A 0.6 HUB-TIP RADIUS-RATIO TRANSONIC TURBINE DESIGNED FOR SECONDARY-FLOW STUDY. II - DESIGN AND EXPERIMENTAL PERFORMANCE OF TURBINE WITH LOW-VELOCITY-TURNING STATOR AND STANDARD ROTORHub-tip radius ratio transonic turbine for secondary flow - turbine with low-velocity turning stator and standard rotor
Document ID
19630002671
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Rohlik, H. E. (NASA Lewis Research Center Cleveland, OH, United States)
Scibbe, H. W. (NASA Lewis Research Center Cleveland, OH, United States)
Wintucky, W. T. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
July 18, 1957
Subject Category
Aircraft
Report/Patent Number
NACA-RM-E57E09
Accession Number
63N12547
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFLOW
TURBINE
STATOR
TRANSONIC FLOW
HUB-TIP RATIO
ROTOR

Related Records

There are no records associated with this record.
No Preview Available