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Pressure Distribution Measurements on a Turbine Rotor Blade Passing Behind a Turbine Nozzle LatticeAs a turbine rotor turns, the blades traverse the wake zones of the nozzle vanes. A periodic fluctuation of the pressure distribution around the circumference of the rotor blade is therefore caused. It was desired to investigate quantitatively this effect. At the same time, the magnitude of the force acting upon one profile of the rotor-blade lattice at various positions of this lattice relative to the nozzle lattice was to be determined.
Document ID
20030068803
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Hausenblas (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 1947
Publication Information
Publication: Berichte der Gittertagung
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NACA-TM-1173
Meeting Information
Meeting: Reports of the Lattice Conference: Berichte der Gittertagung
Location: Brunswick,
Country: Germany
Start Date: March 27, 1944
End Date: March 27, 1944
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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