NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Instrument for measuring the wall shearing stress of turbulent boundary layersIt is shown that at a smooth wall in a turbulent boundary layer the velocity profile next to the wall is dependent, aside from the material constants of the flowing medium, only on the shearing stress transmitted to the wall, even with pressure rise or with pressure drop. Consequently, the heat transfer of a small element that is built into the wall and has a higher temperature than that of the flowing medium is a measure of the wall shearing stress. Theoretical considerations indicate that the wall shearing stress of the boundary layer can be defined by means of a heat-transfer measurement with an instrument mounted in the wall. Such an instrument is described. The calibration curve and its directional sensitivity curve are indicated. It permits the determination of the wall shearing stress in magnitude and direction.
Document ID
19930093956
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ludwieg, H
Date Acquired
August 16, 2013
Publication Date
May 1, 1950
Report/Patent Number
NACA-TM-1284
Report Number: NACA-TM-1284
Accession Number
93R23282
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BOUNDARY LAYER, TURBULENT
BOUNDARY LAYER - TEMPERATURE
INSTRUMENTS - FLOW SHEARING-STRESS INDICATORS
HEAT TRANSMISSION - BOUNDARY LAYER
SKIN FRICTION
BOUNDARY LAYER - WALLS
No Preview Available