NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Flow in Smooth Straight Pipes at Velocities Above and Below Sound VelocityTo investigate the laws of flow of compressible fluids in pipes, tests were carried out with air flowing at velocities below and above that of sound in straight smooth pipes. Air was chosen as the flow medium. In order that the effect of compressibility may be brought out most effectively, the velocity should lie between 100 and 500 m/s (200 and 1,000 mph); that is, be of the order of magnitude of the velocity of sound in air. The behavior of the compression shock in a smooth cylindrical pipe was also investigated. The compression shock can occur at any position in the pipe, depending on the throttling downstream, and travels upstream with increasing throttling up to the pipe entrance, so that only subsonic velocities occur in the pipe.
Document ID
19930094572
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Frossel, W
Date Acquired
September 6, 2013
Publication Date
January 1, 1938
Report/Patent Number
NACA-TM-844
Accession Number
93R23492
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available