Friction Coefficients in the Inlet Length of Smooth Round Tubes
Abstract
An experimental study was made of friction coefficients near the inlet of smooth, round tubes with bellmouth entrances. The tube size ranged from 3/8 inch to 4 inches. Tests were made both with water and with air at low Mach numbers. Near the inlet,the tests indicated a zone in which the developing boundary layer is laminar, followed by a zone in which the boundary layer is turbulent. Transition from a laminar to turbulent boundary layer was found to occur at a Reynolds number of about 5 x 10 sup 5. An approximate method for predicting the discharge coefficient of rounded-entrance flow nozzles, based on the reported results, is presented and is shown to compare well with published data on flow nozzles.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1948
- Accession Number
- ADA801444
Entities
People
- Ascher H. Shapiro
- R. D. Smith
Organizations
- Massachusetts Institute of Technology